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SPACEMOBILE-003, 61045

Orbit data source: Space-Track

SPACEMOBILE-003, 61045 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
61045, 2024-163A
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, 4.5 m
Radar Cross Section
1.500 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 SPACEMOBILE-003
1 61045U 24163A   25240.07620750  .00002892  00000-0  14503-3 0  9999
2 61045  52.9721 217.5835 0010454 328.8791  31.1583 15.20565609 53162
Epoch: 2025-08-28T01:49Z
TLE epoch observation values (Epoch: 2025-08-28T01:49:44.327Z)
Latitude
-0.00004°
Longitude
-146.39563°
Altitude
498.855 km
Speed
7.62 km/s
True Right ascension
14h 30m 20s
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
12:33:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.614 km
Perigee altitude
497.224 km
Semi-major axis
6,882.556 km
Eccentricity
0.00105
Inclination
52.9721°
RAAN
217.5835°
Arg. of periapsis
328.8791°
True anomaly
31.22035°
Mean anomaly
31.1583°
Eccentric anomaly
31.18932°
Mean motion
3.80118 °/min
Orbital period
94.71 mins
BSTAR
0.00014503
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