DECAYED

STARLINK-30238, 57296 (Decayed)

Orbit data source: Space-Track

STARLINK-30238, 57296 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 10 Jul 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.

Not visible in the next 10 days
Identifier
57296, 2023-096G
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)
2023-07-10 (3 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: 4 months ago

TLE from 4 months ago
0 STARLINK-30238
1 57296U 23096G   26055.85190638  .06797521  89360-5  43565-2 0  9990
2 57296  42.9662 211.0200 0023351 319.9929  39.9234 16.15839060146653
Epoch: 2026-02-24T20:26Z
TLE epoch observation values (Epoch: 2026-02-24T20:26:44.711Z)
Latitude
-0°
Longitude
109.60821°
Altitude
218.818 km
Speed
7.784 km/s
True Right ascension
14h 04m 04s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
21:37:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
248.336 km
Perigee altitude
217.461 km
Semi-major axis
6,611.035 km
Eccentricity
0.00234
Inclination
42.9662°
RAAN
211.02°
Arg. of periapsis
319.9929°
True anomaly
40.09551°
Mean anomaly
39.9234°
Eccentric anomaly
40.00942°
Mean motion
4.03775 °/min
Orbital period
89.16 mins
BSTAR
0.0043565
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Computing Atmospheric mass density...

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