First-Move The name MOVE is an acronym that stands for “Munich Orbital Verification Experiment”. Mission After reaching orbit, the first Hauptpayload of the launcher and is ejected after the first CubeSats. Develop only after 15 minutes, the fold-out solar panels … Continue reading →
Built by students at the Kyushu Institute of Technology (KIT) HORYU-2 is 350 * 310 * 315 mm and mass is 7.1 kg. Launched into a Sun-Synchronous 680 km orbit with an inclination of 98.2°and operate on 437.325 MHz using … Continue reading →
HORYU-2 Built by students at the Kyushu Institute of Technology (KIT) HORYU-2 is 350 * 310 * 315 mm and mass is 7.1 kg. It will be launched into a Sun-Synchronous 680 km orbit with an inclination of 98.2°and operate … Continue reading →
Preliminary TLE (Orbital Elements) for the upcoming VEGA launch TLE-new 19-02-2012 12:00 UTC ALMASAT-1 1 38078U 12006B 12049.33443324 .00018909 00000-0 55604-3 0 123 2 38078 69.4856 227.8040 0775179 38.1714 327.1743 14.04552460 692 2012-006C 1 38079U 12006C 12049.75727519 .00032984 00000-0 85788-3 … Continue reading →
Navy-OSCAR 44 (PCSat) Launched September 30, 2001 from the Kodiak Launch Complex on Kodiak Island, Alaska aboard Athena I. Kodiak Star was the first planned orbital launch from the new Kodiak Launch Complex in Alaska was a NASA collaborative mission … Continue reading →
Thanks to the satblog from DK3WN, I saw that Space-Track.com published now the ID’s for the last cubesat launch. DICE 1 1 37851U 11061B 11335.98213095 +.00005465 +00000-0 +44960-3 0 00372 2 37851 101.7084 281.3727 0254523 194.8404 164.5233 14.77965880005103 DICE 2 … Continue reading →