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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 (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: 14 hours ago

TLE from 14 hours ago
0 SPACEMOBILE-003
1 61045U 24163A   26305.65373221  .00000007  00000-0  15141-4 0  9990
2 61045  52.9683  37.4784 0005934 158.1993 201.9255 15.20217226118687
Epoch: 2026-11-01T15:41Z
TLE epoch observation values (Epoch: 2026-11-01T15:41:22.462Z)
Latitude
-0°
Longitude
121.1928°
Altitude
509.849 km
Speed
7.608 km/s
True Right ascension
02h 29m 54s
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
01:22:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.556 km
Perigee altitude
501.386 km
Semi-major axis
6,883.608 km
Eccentricity
0.00059
Inclination
52.9683°
RAAN
37.4784°
Arg. of periapsis
158.1993°
True anomaly
201.90013°
Mean anomaly
201.9255°
Eccentric anomaly
201.91281°
Mean motion
3.80031 °/min
Orbital period
94.73 mins
BSTAR
0.000015141
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Documentation

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