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SPACEMOBILE-002, 61048

Orbit data source: Space-Track

SPACEMOBILE-002, 61048 is a payload satellite owned by AST & Science (US) in LEO that was launched on Thu, 12 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.

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Identifier
61048, 2024-163D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
AST & Science
Mission
Operational Commercial Communications
Bus & Motor
BW3, Unknown motor
Mass
1,500 kg wet, 1,500 kg dry
Launch date (UTC)
Icon of a cake. It is the launch day of the satellite!2024-09-12 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Plate, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)

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

TLE from 11 hours ago
0 SPACEMOBILE-002
1 61048U 24163D   26255.07110481  .00011507  00000-0  53072-3 0  9991
2 61048  52.9654 269.6998 0007226  61.5886 298.5835 15.20683588110987
Epoch: 2026-09-12T01:42Z
TLE epoch observation values (Epoch: 2026-09-12T01:42:23.455Z)
Latitude
-0.00008°
Longitude
-106.98336°
Altitude
502.276 km
Speed
7.616 km/s
True Right ascension
17h 58m 47s
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
05:28:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.037 km
Perigee altitude
499.091 km
Semi-major axis
6,882.201 km
Eccentricity
0.00072
Inclination
52.9654°
RAAN
269.6998°
Arg. of periapsis
61.5886°
True anomaly
298.51076°
Mean anomaly
298.5835°
Eccentric anomaly
298.54713°
Mean motion
3.80147 °/min
Orbital period
94.7 mins
BSTAR
0.00053072
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