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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). 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
61048, 2024-163D
Orbit
LEO
Last TLE update
10 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 10 hours ago
0 SPACEMOBILE-002
1 61048U 24163D   25094.49477773  .00007701  00000-0  36799-3 0  9995
2 61048  52.9767 166.1620 0009786 234.1019 125.9067 15.19927007 31015
Epoch: 2025-04-04T11:52Z
Definitive object data (Epoch: 2025-04-04T11:52:28.795Z)
Latitude
-0.00005°
Longitude
154.98954°
Altitude
510.892 km
Speed
7.607 km/s
True Right ascension
11h 04m 38s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
43.98377°
Longitude
-160.4959°
Altitude
517.194 km
Speed
7.607 km/s
Apparent Right ascension
14h 45m 55s
Apparent Declination
4° 06' 11"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
03:29:46
Azimuth
15.515° NNE
Elevation
-44.842°
Doppler factor
1
Orbital elements
Apogee altitude
513.083 km
Perigee altitude
499.609 km
Semi-major axis
6,884.483 km
Eccentricity
0.0009786
Inclination
52.9767°
RAAN
166.162°
Arg. of periapsis
234.1019°
True anomaly
125.99746°
Mean anomaly
125.9067°
Eccentric anomaly
125.95209°
Mean motion
3.79959 °/min
BSTAR
0.00036799
Orbital period
94.75 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.
6 mins2025-04-05 06:58:26.163Z207.53° SW2025-04-05 07:01:26.163Z148.656° SSE36.391°2025-04-05 07:04:26.163Z65.325° ENE
5 mins2025-04-05 08:38:26.163Z286.84° WNW2025-04-05 08:40:26.163Z332.246° NNW24.889°2025-04-05 08:43:26.163Z29.544° NE
5 mins2025-04-05 13:37:26.163Z330.957° NNW2025-04-05 13:39:26.163Z33.59° NE36.499°2025-04-05 13:42:26.163Z106.212° ESE
4 mins2025-04-05 15:16:26.163Z260.916° W2025-04-05 15:17:26.163Z240.017° WSW20.335°2025-04-05 15:20:26.163Z183.061° SSW
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