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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). Payloads include a variety of satellites, spacecraft, and rockets 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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SPACEMOBILE-002 details
Identifier
61048, 2024-163D
Orbit
LEO
Last TLE update9 hours ago
Origin
Flag of USAST & Science (US)
ManufacturerAST & Science
MissionOperational Commercial Communications
Bus & MotorBW3, Unknown motor
Mass1,500 kg wet, 1,500 kg dry
Launch date (UTC)
2024-09-12 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRBox + 1 Plate, 9 m
Radar Cross Section1.500 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 SPACEMOBILE-002
1 61048U 24163D   25040.23404949  .00006322  00000-0  30983-3 0  9990
2 61048  52.9743  55.1978 0012372  68.2614 291.9695 15.19342384 22766
Epoch: 2025-02-09T05:37Z
Definitive object data (Epoch: 2025-02-09T05:37:01.875Z)
Latitude-0.00007°
Longitude-168.63057°
Altitude505.524 km
Speed7.614 km/s
True Right ascension03h 40m 47s
True Declination0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude-48.83871°
Longitude130.52178°
Altitude531.063 km
Speed7.594 km/s
Apparent Right ascension02h 29m 03s
Apparent Declination-52° 22' 52"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time17:06:12
Azimuth128.22° SE
Elevation-60.53°
Doppler factor1
Orbital elements
Apogee altitude516.632 km
Perigee altitude499.592 km
Semi-major axis6,886.249 km
Eccentricity0.0012372
Inclination52.9743°
RAAN55.1978°
Arg. of periapsis68.2614°
True anomaly291.83795°
Mean anomaly291.9695°
Eccentric anomaly291.90373°
Mean motion3.79812 °/min
BSTAR0.00030983
Orbital period94.78 mins
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SPACEMOBILE-002 Visibility forecast

Observer location: undefined°, undefined

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
4 mins2025-02-10 02:17:53.164Z158.98° S2025-02-10 02:19:53.164Z123.285° SE15.747°2025-02-10 02:21:53.164Z90.207° ESE
5 mins2025-02-10 03:55:53.164Z249.374° W2025-02-10 03:57:53.164Z317.32° NNW41.198°2025-02-10 04:00:53.164Z41.898° NE
5 mins2025-02-10 08:54:53.164Z342.458° N2025-02-10 08:56:53.164Z23.317° NE21.398°2025-02-10 08:59:53.164Z77.709° E
5 mins2025-02-10 10:33:53.164Z297.647° NW2025-02-10 10:35:53.164Z221.453° SW42.168°2025-02-10 10:38:53.164Z143.137° SSE
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