STARLINK-5718, 55620

Orbit data source: Space-Track

STARLINK-5718, 55620 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 12 Feb 2023 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
55620, 2023-020BD
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK, Unknown motor
Mass
305 kg wet, ~290 kg dry
Launch date (UTC)
2023-02-12 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 10.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 STARLINK-5718
1 55620U 23020BD  26061.85202230  .00000593  00000-0  58995-4 0  9999
2 55620  43.0055  28.5666 0001393 265.0635  95.0048 15.02536966168041
Epoch: 2026-03-02T20:26Z
TLE epoch observation values (Epoch: 2026-03-02T20:26:54.726Z)
Latitude
-0.00005°
Longitude
-78.80098°
Altitude
558.939 km
Speed
7.584 km/s
True Right ascension
01h 54m 15s
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
14:48:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.966 km
Perigee altitude
560.033 km
Semi-major axis
6,939.137 km
Eccentricity
0.00014
Inclination
43.0055°
RAAN
28.5666°
Arg. of periapsis
265.0635°
True anomaly
95.0207°
Mean anomaly
95.0048°
Eccentric anomaly
95.01275°
Mean motion
3.75478 °/min
Orbital period
95.88 mins
BSTAR
0.000058995
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|