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SPACEMOBILE-005, 61046

Orbit data source: Space-Track

SPACEMOBILE-005, 61046 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
61046, 2024-163B
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: 18 hours ago

TLE from 18 hours ago
0 SPACEMOBILE-005
1 61046U 24163B   25258.06963657  .00003931  00000-0  19185-3 0  9990
2 61046  52.9759 134.7564 0012210  23.5768 336.5783 15.20545284 55891
Epoch: 2025-09-15T01:40Z
TLE epoch observation values (Epoch: 2025-09-15T01:40:16.599Z)
Latitude
-0.00006°
Longitude
115.40761°
Altitude
497.362 km
Speed
7.621 km/s
True Right ascension
08h 59m 01s
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
12:08:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.883 km
Perigee altitude
496.076 km
Semi-major axis
6,882.617 km
Eccentricity
0.00122
Inclination
52.9759°
RAAN
134.7564°
Arg. of periapsis
23.5768°
True anomaly
336.52261°
Mean anomaly
336.5783°
Eccentric anomaly
336.55046°
Mean motion
3.80113 °/min
Orbital period
94.71 mins
BSTAR
0.00019185
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