{"result":"*******************************************************************************\n Revised: Dec 07, 2022      OMOTENASHI / Spacecraft (Moon)                 -75\n                 https://www.isas.jaxa.jp/home/omotenashi/index.html\nhttps://directory.eoportal.org/web/eoportal/satellite-missions/content/-/article/equuleus-and-omotenashi\n\n NOTE: Communications with this spacecraft were unreliable after deployment. \n  It is believed the solar panels did not successfully point to the Sun. \n  Recovery attempts ended November 22 when JAXA determined it could not \n  perform the lunar mission. \n\n BACKGROUND:\n  The \"Outstanding MOon exploration TEchnologies demonstrated by NAno Semi-Hard\n   Impactor (OMOTENASHI), is a 6U Cubesat built by JAXA. It was carried with \n   the Orion EM-1 (Exploration Mission-1) into a heliocentric orbit in \n   cislunar space on the maiden flight of the NASA SLS (Space Launch System)\n\n  The goal is to demonstrate a low-cost technology for semi-hard landing on \n   the Moon's surface after being deployed in a lunar fly-by orbit\n\n  After deploying from SLS, OMOTENASHI will perform two deterministic maneuvers:\n\n   DV1: will separate from the Orbiting Module (OM) and inject OMOTENASHI\n        onto a Moon-impacting trajectory.\n\n  After midcourse Trajectory Correction Maneuvers (TCMs) as needed ...\n\n   DV2: a solid rocket motor will then be ignited shortly before lunar \n        collision, when moving at a speed of approximately 2.5 km/s. \n\n  After the deceleration maneuver (DV2), OMOTENASHI will free-fall from a low \n  altitude (~100 m) and arrive at the Moon surface with a speed of 20-30 m/s.\n\n SPACECRAFT PHYSICAL CHARACTERISTICS:\n   * Dimensions          : 10.0 x 22.73 x 36.6 cm (6U CubeSat)\n   * Orbiting Module (OM): 8.6 kg \n   * Surface Probe (SP)  : 0.7 kg (airbag)\n   * Retro motor (RM)    : 4.4 kg (decelerates Surface Probe to surface)\n   * Total mass          : 14 kg\n   * Communications      : X-band, UHF (amateur radio accessible)\n\n SPACECRAFT TRAJECTORY:\n  Post-launch reconstruction trajectory from JAXA.\n\n  Trajectory name                         Start (TDB)        Stop (TDB)\n  -------------------------------     -----------------  -----------------\n  20221116_0155_0100_V0.1             2022-Nov-16 10:33  2023-Mar-31 23:59\n*******************************************************************************\n","signature":{"version":"1.2","source":"NASA/JPL Horizons API"}}