STARLINK-37289, 68545

Orbit data source: Space-Track

STARLINK-37289, 68545 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Apr 2026 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
68545, 2026-070D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
2026-04-02 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 STARLINK-37289
1 68545U 26070D   26247.14833556  .00015357  00000-0  46459-3 0  9991
2 68545  53.1586 250.3982 0001285 111.4627 248.6512 15.34408674 23921
Epoch: 2026-09-04T03:33Z
TLE epoch observation values (Epoch: 2026-09-04T03:33:36.192Z)
Latitude
-0.00007°
Longitude
-146.27897°
Altitude
463.899 km
Speed
7.636 km/s
True Right ascension
16h 41m 35s
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
01:36:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.814 km
Perigee altitude
462.055 km
Semi-major axis
6,841.072 km
Eccentricity
0.00013
Inclination
53.1586°
RAAN
250.3982°
Arg. of periapsis
111.4627°
True anomaly
248.63749°
Mean anomaly
248.6512°
Eccentric anomaly
248.64434°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00046459
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
|