JCAT SatcatLaunch_Tag Piece Type Name PLName LDate Parent SDate Primary DDate Status Dest Owner State Manufacturer Bus Motor Mass DryMass TotMass Length Diamete Span Shape ODate Perigee Apogee Inc OpOrbitOQU AltNames
# Updated 2025 Jul 11 0128:42
T00001 NNA 2025-135 2025-135BT P ? ICEYE-X57 ICEYE-X57 2025 Jun 23 A11534 2025 Jun 23 2350 Earth - O - ICEUS US ICEYE ICEYE - 80 80 80 0.8 0.6 1.5 ? Box + pan - 0 0 0.00 - -
T00002 NNA 2025-038 2025-038 P D Cubesat Cubesat 2025 Feb 27 S63102 2025 Feb 27 0105 Earth - AO - UNKUS US SPINV Cubesat 16U - 20 ? 20 ? 20 ? 0.4 0.4 0.4 Box - 0 0 0.00 - -
T00003
T00004
T00005
T00006 NNA 2025-052 2025-052BS P ? Tevel 2-6 Tevel 2-6 2025 Mar 15 A11437 2025 Mar 15 0739 Earth - O - TAU/ISA IL ISA/TAU Cubesat 1U - 1 1 1 0.1 0.1 0.1 Box 2025 Mar 28 512 517 97.45 LLEO/S -
T00007 NNA 2025-135 2025-135BU P ? Lemur-2 Lacunasat 2025 Jun 22 S64587 2025 Jun 22 Earth - AO - SPIRE/LACU US SPIREG Cubesat 4U - 5 5 5 0.4 0.1 0.4 Box - 0 0 0.00 - -
T00008 NNA 2025-135 2025-135BV P ? Lemur-2 Lacunasat 2025 Jun 22 S64587 2025 Jun 22 Earth - AO - SPIRE/LACU US SPIREG Cubesat 4U - 5 5 5 0.4 0.1 0.4 Box - 0 0 0.00 - -
T00009
T00010
T00011 NNA 2025-052 2025-052BT P ? Tevel 2-5 Tevel 2-5 2025 Mar 15 A11437 2025 Mar 15 0739 Earth - O - TAU/ISA IL ISA/TAU Cubesat 1U - 1 1 1 0.1 0.1 0.1 Box 2025 Mar 28 511 517 97.45 LLEO/S -
T00012
T00013
T00014 NNA 2025-082 2025-082 CP T T Shenzhou 20 Guidao Cang Shenzhou 20 orbital module 2025 Apr 24 S63632 2025 Apr 24 0927:07 Earth - AO - CMSEO CN CAST Shenzhou OM - 1842 ? 1500 ? 1842 ? 2.3 2.8 4.3 Cyl + 2 pan - 0 0 0.00 - -
T00015
T00016
T00017
T00018
T00019
T00020
T00021 71304 2025-009 2025-009DU P ? Flock 4g-19 Dove 24d4 2025 Jan 14 A11398 2025 Jan 14 2003:57 Earth - O - PLAN US PLAN Cubesat 3U - 5.700 5.700 5.700 0.3 0.1 0.3 Box+2 pan 2025 Jan 19 512 520 97.44 LLEO/S -
T00022
T00023 NNA 2024-043 2024-043 P ? Gluon Gluon 2024 Mar 4 S59119 2024 Mar 4 2318:43 Earth - AO - ATOMOS US ATOMOS Atomos - 100 ? 100 ? 100 ? 0.5 1.0 1.0 Box + 2 pan - 0 0 0.00 - -