[ hide orbit diagram ]
For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.
Orbital Elements at Epoch 2453141.5 (2004-May-16.0) TDB
Reference: JPL 207 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | 1.000688204104655 | 9.6998e-07 | |
a | -1397.782599782068 | 1.97 | au |
q | .9619597225853242 | 9.1376e-08 | au |
i | 99.64263544704116 | 8.5227e-06 | deg |
node | 210.278431108308 | 1.0385e-05 | deg |
peri | 1.204334608020704 | 1.0881e-05 | deg |
M | 6.468919385957737E-7 | 1.4431e-09 | deg |
tp | 2453141.465700553637 (2004-May-15.96570055) | 8.8899e-06 | TDB |
period | n/a n/a | n/a n/a | d yr |
n | 1.886012770438181E-5 | 3.9872e-08 | deg/d |
Q | n/a | n/a | au |
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Additional Model Parameters
Parameter | Value | Uncertainty (1-sigma) |
A1 [EST] | 1.635562356445317E-8 | 1.566E-10 |
A2 [EST] | 4.916600112437359E-10 | 7.526E-11 |
A3 [EST] | 4.929063627255129E-10 | 6.246E-11 |
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| | Orbit Determination Parameters
Additional Information
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[ hide covariance matrix ]
Orbit Covariance (9×9)
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|
e |
q |
tp |
node |
peri |
i |
A1 |
A2 |
A3 |
e |
9.408598054802967E-13 |
4.003105652310874E-14 |
-3.46422039587932E-12 |
-3.703068063183188E-12 |
-5.471471163398125E-12 |
1.175008686381379E-12 |
-1.4610893814305E-16 |
-1.506219399847174E-17 |
9.012115734108406E-18 |
q |
4.003105652310874E-14 |
8.349643494873292E-15 |
-1.088021302512134E-13 |
-1.699629202540789E-13 |
-1.506510513560184E-13 |
6.794457789347159E-14 |
-7.299824426406371E-18 |
-3.092458368324504E-19 |
4.096927672974398E-19 |
tp |
-3.46422039587932E-12 |
-1.088021302512134E-13 |
7.903041725002196E-11 |
1.520506929285308E-11 |
8.3789317058417E-11 |
-1.210402200967455E-11 |
5.821587870354928E-16 |
2.481410855800861E-16 |
-4.182057974577954E-17 |
node |
-3.703068063183188E-12 |
-1.699629202540789E-13 |
1.520506929285308E-11 |
1.078399728222579E-10 |
3.917011098891049E-11 |
-6.838916810801562E-12 |
5.624771511998056E-16 |
1.927381441673533E-17 |
-2.768603332579411E-16 |
peri |
-5.471471163398125E-12 |
-1.506510513560184E-13 |
8.3789317058417E-11 |
3.917011098891049E-11 |
1.183884036321815E-10 |
-1.074873402945005E-11 |
9.015452408102109E-16 |
3.010741710163661E-16 |
-1.108120356518942E-16 |
i |
1.175008686381379E-12 |
6.794457789347159E-14 |
-1.210402200967455E-11 |
-6.838916810801562E-12 |
-1.074873402945005E-11 |
7.263577953074637E-11 |
-1.749406552689769E-16 |
-1.816665403244446E-17 |
-1.189522733609553E-16 |
A1 |
-1.4610893814305E-16 |
-7.299824426406371E-18 |
5.821587870354928E-16 |
5.624771511998056E-16 |
9.015452408102109E-16 |
-1.749406552689769E-16 |
2.451271173471826E-20 |
3.425028402475219E-21 |
-1.423028646879039E-21 |
A2 |
-1.506219399847174E-17 |
-3.092458368324504E-19 |
2.481410855800861E-16 |
1.927381441673533E-17 |
3.010741710163661E-16 |
-1.816665403244446E-17 |
3.425028402475219E-21 |
5.664217207178204E-21 |
-2.21414245809971E-22 |
A3 |
9.012115734108406E-18 |
4.096927672974398E-19 |
-4.182057974577954E-17 |
-2.768603332579411E-16 |
-1.108120356518942E-16 |
-1.189522733609553E-16 |
-1.423028646879039E-21 |
-2.21414245809971E-22 |
3.901417930799407E-21 |
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[ hide close-approach data ]
Close-Approach Data ...sorted by Date/Time (TDB)
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Date/Time (TDB) |
Time Uncertainty (days_HH:MM) |
Body |
Nominal Distance (au) |
Minimum Distance (au) |
Maximum Distance (au) |
V-relative (km/s) |
V-infinity (km/s) |
JD (TDB) |
Time Uncertainty (minutes) |
Semi-major axis (km) |
Semi-minor axis (km) |
range-LOV angle (deg) |
N-sigma |
BP |
Orbit Ref. |
Reference |
Modified |
2004-May-06 17:45 |
< 00:01 |
Earth |
0.320960799167257 |
0.32096029696327 |
0.320961301371245 |
56.2057342815981 |
56.2055865816615 |
2453132.239675626 |
0.00587657941876261 |
25.4754347675159 |
16.0538399693283 |
13.6698229864554 |
1953990.5081087 |
T |
207 |
CATAB v2.0e-lin.ifort 2017-Nov-30 18:58:56 |
2017-Nov-30 18:58 |
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