Launch Details

Launched	29 March 2026
Flight ended	–
Status	Operational
Category	Active satellites
Launch site	Air Force Western Test Range, California, USA
Owner	Spain
NORAD ID	68478
COSPAR ID	2026-067BQ
Observing

Current orbital elements

Inclination	97.760°
Eccentricity	0.00002
RA ascending node	8.787 hr
Argument perigee	264.938°
Mean anomaly	95.181°
Orbital period	96.506 min
Epoch of osculation	22 Jun 2026, 14:19

See historical orbital elements »

Derived Quantities

Min Altitude	598.2 km
Mean Altitude	598.4 km
Peak Altitude	598.5 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 W-SERIES 6 LUNA-2 LEMUR-2-DELOITTE-3 FLYLAB1 VIGORIDE-7 BLACK KITE-2 UNICORN-2S LEMUR-2-JULIA-JOEL TRANSPORTER-16 OBJECT BP 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