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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). 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
61047, 2024-163C
Orbit
LEO
Last TLE update
14 hours ago
Origin
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 (7 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Plate, 9 m
Radar Cross Section
1.500 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 14 hours ago
0 SPACEMOBILE-001
1 61047U 24163C   25094.51193388  .00006827  00000-0  32808-3 0  9999
2 61047  52.9692 166.2016 0010261 228.8788 131.1320 15.19912255 31014
Epoch: 2025-04-04T12:17Z
Definitive object data (Epoch: 2025-04-04T12:17:11.087Z)
Latitude
-0.00006°
Longitude
148.836°
Altitude
511.631 km
Speed
7.607 km/s
True Right ascension
11h 04m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
-49.7811°
Longitude
83.65397°
Altitude
519.351 km
Speed
7.606 km/s
Apparent Right ascension
00h 25m 06s
Apparent Declination
-79° 44' 10"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
08:04:21
Azimuth
192.89° SSW
Elevation
-43.531°
Doppler factor
1
Orbital elements
Apogee altitude
513.456 km
Perigee altitude
499.327 km
Semi-major axis
6,884.529 km
Eccentricity
0.0010261
Inclination
52.9692°
RAAN
166.2016°
Arg. of periapsis
228.8788°
True anomaly
131.22049°
Mean anomaly
131.132°
Eccentric anomaly
131.17625°
Mean motion
3.79955 °/min
BSTAR
0.00032808
Orbital period
94.75 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 mins2025-04-05 07:24:15.882Z226.295° WSW2025-04-05 07:27:15.882Z171.267° S44.759°2025-04-05 07:30:15.882Z52.123° ENE
4 mins2025-04-05 09:05:15.882Z313.869° NW2025-04-05 09:06:15.882Z335.158° NNW19.567°2025-04-05 09:09:15.882Z26.978° NE
5 mins2025-04-05 14:03:15.882Z315.792° NNW2025-04-05 14:05:15.882Z50.026° ENE44.33°2025-04-05 14:08:15.882Z124.815° SE
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