STARLINK-32156, 60278

Orbit data source: Space-Track

STARLINK-32156, 60278 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 28 Jul 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.

Loading next visibility...
Identifier
60278, 2024-132A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
2024-07-28 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)

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

TLE from 15 hours ago
0 STARLINK-32156
1 60278U 24132A   26062.43258582 -.00000103  00000-0  86642-5 0  9994
2 60278  53.1612  81.4061 0001705  89.6805 270.4391 15.30193466 91826
Epoch: 2026-03-03T10:22Z
TLE epoch observation values (Epoch: 2026-03-03T10:22:55.414Z)
Latitude
-0.00005°
Longitude
124.46344°
Altitude
476.126 km
Speed
7.629 km/s
True Right ascension
05h 25m 37s
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
05:14:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.659 km
Perigee altitude
474.322 km
Semi-major axis
6,853.628 km
Eccentricity
0.00017
Inclination
53.1612°
RAAN
81.4061°
Arg. of periapsis
89.6805°
True anomaly
270.41956°
Mean anomaly
270.4391°
Eccentric anomaly
270.42933°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.0000086642
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
|