DECAYED

STARLINK-1408, 45688 (Decayed)

Orbit data source: Space-Track

STARLINK-1408, 45688 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 04 Jun 2020 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.

Not visible in the next 10 days
Identifier
45688, 2020-035AH
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Decayed Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
260 kg wet, ~248 kg dry
Launch date (UTC)
2020-06-04 (6 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 STARLINK-1408
1 45688U 20035AH  25061.57211343  .11786900  12454-4  69872-3 0  9998
2 45688  53.0464 117.7483 0002904  12.2568 149.0371 16.41661657264779
Epoch: 2025-03-02T13:43Z
TLE epoch observation values (Epoch: 2025-03-02T13:43:50.600Z)
Latitude
14.84962°
Longitude
-80.25303°
Altitude
163.215 km
Speed
7.81 km/s
True Right ascension
19h 05m 14s
True Declination
14° 45' 25"
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
14:04:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.573 km
Perigee altitude
159.774 km
Semi-major axis
6,539.811 km
Eccentricity
0.00029
Inclination
53.0464°
RAAN
117.7483°
Arg. of periapsis
12.2568°
True anomaly
149.05422°
Mean anomaly
149.0371°
Eccentric anomaly
149.04566°
Mean motion
4.10389 °/min
Orbital period
87.72 mins
BSTAR
0.00069872
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|