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GRUS-3G, 69878

Orbit data source: Space-Track

GRUS-3G, 69878 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
69878, 2026-156K
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 (2 months 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: 8 hours ago

TLE from 8 hours ago
0 GRUS-3G
1 69878U 26156K   26237.17422424  .00000681  00000-0  73057-4 0  9995
2 69878  97.7458 136.8012 0006728   1.3288 358.7947 14.91772530  7285
Epoch: 2026-08-25T04:10Z
TLE epoch observation values (Epoch: 2026-08-25T04:10:52.974Z)
Latitude
-0.00006°
Longitude
100.63512°
Altitude
590.761 km
Speed
7.567 km/s
True Right ascension
09h 07m 12s
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
03:49:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.115 km
Perigee altitude
584.739 km
Semi-major axis
6,967.564 km
Eccentricity
0.00067
Inclination
97.7458°
RAAN
136.8012°
Arg. of periapsis
1.3288°
True anomaly
358.79308°
Mean anomaly
358.7947°
Eccentric anomaly
358.79389°
Mean motion
3.73183 °/min
Orbital period
96.47 mins
BSTAR
0.000073057
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