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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)
2024-09-12 (1 year 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   26035.77952259  .00016255  00000-0  73028-3 0  9999
2 61048  52.9694 198.1770 0009660  93.9879 266.2220 15.21269979 77617
Epoch: 2026-02-04T18:42Z
TLE epoch observation values (Epoch: 2026-02-04T18:42:30.751Z)
Latitude
-0.00002°
Longitude
142.60765°
Altitude
503.329 km
Speed
7.614 km/s
True Right ascension
13h 12m 42s
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
08:13:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.941 km
Perigee altitude
495.649 km
Semi-major axis
6,880.432 km
Eccentricity
0.00097
Inclination
52.9694°
RAAN
198.177°
Arg. of periapsis
93.9879°
True anomaly
266.11155°
Mean anomaly
266.222°
Eccentric anomaly
266.16678°
Mean motion
3.80294 °/min
Orbital period
94.66 mins
BSTAR
0.00073028
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Documentation

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