Showing default

GRUS-3B, 69918

Orbit data source: Space-Track

GRUS-3B, 69918 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
69918, 2026-156BB
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-3B
1 69918U 26156BB  26211.28230955  .00001104  00000-0  11509-3 0  9994
2 69918  97.7539 111.3661 0007901  80.3151 279.8960 14.91756751  3425
Epoch: 2026-07-30T06:46Z
TLE epoch observation values (Epoch: 2026-07-30T06:46:31.545Z)
Latitude
0.00001°
Longitude
61.8096°
Altitude
594.557 km
Speed
7.563 km/s
True Right ascension
07h 25m 27s
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
14:47:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.981 km
Perigee altitude
583.971 km
Semi-major axis
6,967.613 km
Eccentricity
0.00079
Inclination
97.7539°
RAAN
111.3661°
Arg. of periapsis
80.3151°
True anomaly
279.80679°
Mean anomaly
279.896°
Eccentric anomaly
279.8514°
Mean motion
3.73179 °/min
Orbital period
96.47 mins
BSTAR
0.00011509
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
|