Showing default

GRUS-3D, 69919

Orbit data source: Space-Track

GRUS-3D, 69919 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.

Loading next visibility...
Identifier
69919, 2026-156BC
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
RCS unknown

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

TLE from 18 hours ago
0 GRUS-3D
1 69919U 26156BC  26211.28033382  .00001143  00000-0  11859-3 0  9991
2 69919  97.7507 111.3586 0008720  79.4494 280.7707 14.91885649  3425
Epoch: 2026-07-30T06:43Z
TLE epoch observation values (Epoch: 2026-07-30T06:43:40.842Z)
Latitude
0.00002°
Longitude
62.5153°
Altitude
593.967 km
Speed
7.564 km/s
True Right ascension
07h 25m 26s
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
14:10:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.15 km
Perigee altitude
582.999 km
Semi-major axis
6,967.212 km
Eccentricity
0.00087
Inclination
97.7507°
RAAN
111.3586°
Arg. of periapsis
79.4494°
True anomaly
280.67252°
Mean anomaly
280.7707°
Eccentric anomaly
280.72161°
Mean motion
3.73211 °/min
Orbital period
96.46 mins
BSTAR
0.00011859
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|