JCAT Satcat Launch_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 2026 Mar 21 1649:13
T00001
T00002
T00003
T00004
T00005 NNA 2025-313 2025-313 P Trisat-4 Trisat-4 2025 Dec 28 S67286 2025 Dec 28 Earth - O - OKB5P RU OKB5P Trisat - 0.500 0.500 0.500 0.010 0.3 0.3 Plate 2026 Jan 8 494 510 97.41 LLEO/S -
T00006
T00007
T00008
T00009
T00010
T00011
T00012
T00013
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T00015
T00016 NNA 2025-272 2025-272 CP T T Shenzhou 22 Guidao Cang Shenzhou 22 orbital module 2025 Nov 25 S66645 2025 Nov 25 0421 Earth - AO - CMSEO CN CAST Shenzhou OM - 1842 ? 1500 ? 1842 ? 2.3 2.8 4.3 Cyl + 2 pan - 0 0 0.00 - -
T00017 NNA 2025-274 2025-274Q P ? Duri SNUGLITE-III 2025 Nov 26 S66661 2025 Dec 4? Earth - AO - SNU KR SNU Cubesat 3U - 3.600 3.600 3.600 0.3 0.1 0.3 Box - 0 0 0.00 - -
T00018
T00019
T00020
T00021
T00022
T00023 NNA 2025-276 2025-276DZ P ? 3UCUBED-A 3UCUBED-A 2025 Nov 28 A11695 2025 Nov 28 1948:21 Earth - O - UNH US UNH Cubesat 3U - 5 5 5 0.3 0.1 0.3 Box 2025 Dec 18 514 518 97.44 LLEO/S -
T00024
T00025
T00026
T00027
T00028
T00029 NNA 2025-276 2025-276EF P ? Lemur-2 Tartiflette Lemur-2 2025 Nov 28 A11698 2026 Feb 16? Earth - O - SPIRE US SPIREG Cubesat 3U - 7.600 7.600 7.600 0.3 0.1 1.0 Box+ 2 pan - 0 0 0.00 - -
T00030 NNA 2025-276 2025-276EG P ? Lemur-2 Hotspur-Tom Lemur-2 2025 Nov 28 A11699 2026 Feb 19? Earth - O - SPIRE US SPIREG Cubesat 3U - 7.600 7.600 7.600 0.3 0.1 1.0 Box+ 2 pan - 0 0 0.00 - -