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SPACEMOBILE-001, 61047

Orbit data source: Space-Track

SPACEMOBILE-001, 61047 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-001 details
Identifier
61047, 2024-163C
Orbit
LEO
Last TLE update1 day 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 1 day ago
0 SPACEMOBILE-001
1 61047U 24163C   25042.48703409  .00007191  00000-0  35033-3 0  9997
2 61047  52.9754  44.9864 0013328  70.3548 289.8883 15.19327614 23102
Epoch: 2025-02-11T11:41Z
Definitive object data (Epoch: 2025-02-11T11:41:19.745Z)
Latitude0.00001°
Longitude87.86298°
Altitude505.636 km
Speed7.614 km/s
True Right ascension02h 59m 56s
True Declination0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude22.76469°
Longitude101.05273°
Altitude502.021 km
Speed7.62 km/s
Apparent Right ascension04h 26m 28s
Apparent Declination-7° 19' 04"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time17:10:20
Azimuth19.695° NNE
Elevation-55.953°
Doppler factor1
Orbital elements
Apogee altitude517.334 km
Perigee altitude498.978 km
Semi-major axis6,886.293 km
Eccentricity0.0013328
Inclination52.9754°
RAAN44.9864°
Arg. of periapsis70.3548°
True anomaly289.7446°
Mean anomaly289.8883°
Eccentric anomaly289.81646°
Mean motion3.79809 °/min
BSTAR0.00035033
Orbital period94.78 mins
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SPACEMOBILE-001 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.
6 mins2025-02-13 01:44:13.311Z191.997° SSW2025-02-13 01:47:13.311Z125.577° SE28.178°2025-02-13 01:50:13.311Z69.568° E
5 mins2025-02-13 03:23:13.311Z271.415° WNW2025-02-13 03:25:13.311Z314.263° NW28.702°2025-02-13 03:28:13.311Z28.738° NE
6 mins2025-02-13 08:22:13.311Z331.447° NNW2025-02-13 08:25:13.311Z49.279° ENE29.242°2025-02-13 08:28:13.311Z98.933° ESE
5 mins2025-02-13 10:01:13.311Z278.577° WNW2025-02-13 10:03:13.311Z231.372° WSW27.355°2025-02-13 10:06:13.311Z168.84° S
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