Launch Details

Launched	29 March 2026
Flight ended	–
Status	Operational
Category	Active satellites
Launch site	Air Force Western Test Range, California, USA
Owner
NORAD ID	68462
COSPAR ID	2026-067AY
Observing

Current orbital elements

Inclination	97.453°
Eccentricity	0.00030
RA ascending node	5.376 hr
Argument perigee	146.125°
Mean anomaly	214.017°
Orbital period	94.856 min
Epoch of osculation	01 May 2026, 11:23

See historical orbital elements »

Derived Quantities

Min Altitude	516.7 km
Mean Altitude	518.8 km
Peak Altitude	520.8 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 TRANSPORTER-16 OBJECT M OUT OF THE BOX TRANSPORTER-16 OBJECT P TRANSPORTER-16 OBJECT Q DISCO-2 TRANSPORTER-16 OBJECT S T.MICROSAT-2 VIREON-1 ION SCV-019 HAWK-14B TRANSPORTER-16 OBJECT X TRANSPORTER-16 OBJECT Y TRANSPORTER-16 OBJECT Z TRANSPORTER-16 OBJECT AA HAWK-14C TRANSPORTER-16 OBJECT AC TRANSPORTER-16 OBJECT AD TRANSPORTER-16 OBJECT AE TRANSPORTER-16 OBJECT AF HADES-SA TRANSPORTER-16 OBJECT AH HAWK-14A TRANSPORTER-16 OBJECT AK TRANSPORTER-16 OBJECT AL TRANSPORTER-16 OBJECT AM TRANSPORTER-16 OBJECT AN TRANSPORTER-16 OBJECT AP TRANSPORTER-16 OBJECT AQ TRANSPORTER-16 OBJECT AR PARUS-6U1 TRANSPORTER-16 OBJECT AT SAL-E TRANSPORTER-16 OBJECT AV COSMO TRANSPORTER-16 OBJECT AX GARAI-B FGN-100-D3 HOTSAT-2 TRANSPORTER-16 OBJECT BC TRANSPORTER-16 OBJECT BD ERMIS-1 TRANSPORTER-16 OBJECT BF TRANSPORTER-16 OBJECT BG LEMUR-2-DELOITTE-3 FLYLAB1 TRANSPORTER-16 OBJECT BK BLACK KITE-2 TRANSPORTER-16 OBJECT BM 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 TRANSPORTER-16 OBJECT BX VINDLER 2.3 TRANSPORTER-16 OBJECT BZ VINDLER 2.1 LEMUR-2-CARROLLEMO TRANSPORTER-16 OBJECT CC 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