Launch Details

Launched	29 March 2026
Flight ended	18 May 2026
Status	Decayed
Launch site	Air Force Western Test Range, California, USA
Owner	United States
NORAD ID	68469
COSPAR ID	2026-067BF
Observing

Current orbital elements

Inclination	97.451°
Eccentricity	0.04204
RA ascending node	6.544 hr
Argument perigee	19.638°
Mean anomaly	264.422°
Orbital period	96.619 min
Epoch of osculation	19 May 2026, 06:00

See historical orbital elements »

Derived Quantities

Min Altitude	310.6 km
Mean Altitude	603.9 km
Peak Altitude	897.1 km

Launched alongside

TRANSPORTER-16 OBJECT A JACK-002 OPTISAT FEMTO-1 ERMIS-2 VIREON-2 BRO-19 SPOQC SPACEVAN-002 ERMIS-3 TRANSPORTER-16 OBJECT L EMISAR OUT OF THE BOX TROOP-F3 VEGAFLY-1 DISCO-2 NUSAT-53 T.MICROSAT-2 VIREON-1 ION SCV-019 HAWK-14B AIGLONSAT-1 TRANSPORTER-16 OBJECT Y TRANSPORTER-16 OBJECT Z TRANSPORTER-16 OBJECT AA HAWK-14C NUSAT-54 DB-WALI-WMU SHARJAH-SAT-2 DB SKYFORGE CORE TU HADES-SA IRIDE-MS1-EAGLET 2-14 HAWK-14A IRIDE-MS1-EAGLET 2-9 IRIDE-MS1-EAGLET 2-13 IRIDE-MS1-EAGLET 2-10 IRIDE-MS1-EAGLET 2-16 IRIDE-MS1-EAGLET 2-11 AISSAT 4 DB CHARMS ND PARUS-6U1 TRANSPORTER-16 OBJECT AT SAL-E DB GME UT COSMO IRIDE-MS1-EAGLET 2-12 IRIDE-MS1-EAGLET 2-15 GARAI-B FGN-100-D3 HOTSAT-2 DB-PFW TRANSPORTER-16 OBJECT BD ERMIS-1 LUNA-2 LEMUR-2-DELOITTE-3 FLYLAB1 VIGORIDE-7 BLACK KITE-2 UNICORN-2S LEMUR-2-JULIA-JOEL TRANSPORTER-16 OBJECT BP FOSSASAT-2E25 LEMUR-2-PEGGY-2004 LEMUR-2-IRINA TORO3 LEMUR-2-SEJONG-3 LEMUR-2-CLARA VINDLER 2.2 CAPELLA-20 VINDLER 2.3 AE1A VINDLER 2.1 LEMUR-2-CARROLLEMO MIMIR 1 LEMUR-2-DELOITTE-2 LEMUR-2-EMARCHIA LEMUR-2-POLO-11 ICEYE-X71 GRAVITAS ICEYE-X73 ICEYE-X75 IO-1 SERT3 ICEYE-X74 TRANSPORTER-16 OBJECT CP ICEYE-X76 FLYLAB2 ICEYE-X72 GEMS2-AMETHYST AEPEX CAMOES MARS-1 BESSA