SPACEMOBILE-003, 61045
Orbit data source: Space-Track
SPACEMOBILE-003, 61045 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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61045 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Plate, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 25321.69987464 .00000200 00000-0 23617-4 0 9993
2 61045 52.9792 202.2667 0009842 197.3569 162.7090 15.20978766 65580Epoch: 2025-11-17T16:47Z
TLE epoch observation values (Epoch: 2025-11-17T16:47:49.168Z)
Latitude
-0.00006°
Longitude
-106.68477°
Altitude
510.23 km
Speed
7.606 km/s
True Right ascension
13h 29m 03s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:03:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.944 km
Perigee altitude
496.399 km
Semi-major axis
6,881.309 km
Eccentricity
0.00098
Inclination
52.9792°
RAAN
202.2667°
Arg. of periapsis
197.3569°
True anomaly
162.74248°
Mean anomaly
162.709°
Eccentric anomaly
162.72574°
Mean motion
3.80221 °/min
Orbital period
94.68 mins
BSTAR
0.000023617
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SPACEMOBILE-003 Visibility forecast
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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 mins | 2025-11-18 18:11:12.966Z | 199.8° SSW | 2025-11-18 18:14:12.966Z | 139.719° SSE | 31.881° | 2025-11-18 18:17:12.966Z | 69.282° E |
| 5 mins | 2025-11-18 19:51:12.966Z | 285.309° WNW | 2025-11-18 19:53:12.966Z | 339.052° N | 27.221° | 2025-11-18 19:56:12.966Z | 33.201° NE |
| 6 mins | 2025-11-19 00:49:12.966Z | 329.231° NNW | 2025-11-19 00:52:12.966Z | 51.631° ENE | 31.583° | 2025-11-19 00:55:12.966Z | 102.623° ESE |
| 5 mins | 2025-11-19 02:28:12.966Z | 273.688° WNW | 2025-11-19 02:30:12.966Z | 227.874° WSW | 24.396° | 2025-11-19 02:33:12.966Z | 172.143° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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