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GRUS-3A, 69885

Orbit data source: Space-Track

GRUS-3A, 69885 is a payload satellite owned by AXELSPACE (JP) in SSO that was launched on Tue, 07 Jul 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
69885, 2026-156S
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
AXELSPACE
Mission
Operational spacecraft
Bus & Motor
GRUS, Unknown motor
Mass
150 kg wet, 150 kg dry
Launch date (UTC)
2026-07-07 (3 weeks ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
BOX, 1.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 GRUS-3A
1 69885U 26156S   26211.28685939  .00001018  00000-0  10735-3 0  9997
2 69885  97.7506 111.3497 0007320  70.3711 289.8297 14.91460055  3428
Epoch: 2026-07-30T06:53Z
TLE epoch observation values (Epoch: 2026-07-30T06:53:04.651Z)
Latitude
-0.00002°
Longitude
60.15077°
Altitude
594.695 km
Speed
7.563 km/s
True Right ascension
07h 25m 23s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:48:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.502 km
Perigee altitude
585.3 km
Semi-major axis
6,968.538 km
Eccentricity
0.00073
Inclination
97.7506°
RAAN
111.3497°
Arg. of periapsis
70.3711°
True anomaly
289.75077°
Mean anomaly
289.8297°
Eccentric anomaly
289.79024°
Mean motion
3.73105 °/min
Orbital period
96.49 mins
BSTAR
0.00010735
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