DECAYED

STARLINK-11278, 60990 (Decayed)

Orbit data source: Space-Track

STARLINK-11278, 60990 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 05 Sep 2024 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
60990, 2024-158A
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Decayed Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
2024-09-05 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 STARLINK-11278
1 60990U 24158A   24256.92781948  .45865837  12647-4  35492-3 0  9997
2 60990  53.1497  77.5570 0005192 232.2397 278.1431 16.52258777  1345
Epoch: 2024-09-12T22:16Z
TLE epoch observation values (Epoch: 2024-09-12T22:16:03.603Z)
Latitude
23.40346°
Longitude
-87.67944°
Altitude
133.732 km
Speed
7.83 km/s
True Right ascension
15h 54m 58s
True Declination
23° 15' 59"
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
09:22:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
137.046 km
Perigee altitude
130.285 km
Semi-major axis
6,511.802 km
Eccentricity
0.00052
Inclination
53.1497°
RAAN
77.557°
Arg. of periapsis
232.2397°
True anomaly
278.0842°
Mean anomaly
278.1431°
Eccentric anomaly
278.11365°
Mean motion
4.13039 °/min
Orbital period
87.16 mins
BSTAR
0.00035492
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
|