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: 16 hours ago
TLE from 16 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 25354.42428624 .00009270 00000-0 42732-3 0 9992
2 61045 52.9709 51.7583 0008244 311.6703 48.3585 15.20936658 70564Epoch: 2025-12-20T10:10Z
TLE epoch observation values (Epoch: 2025-12-20T10:10:58.331Z)
Latitude
0°
Longitude
169.76397°
Altitude
500.123 km
Speed
7.618 km/s
True Right ascension
03h 27m 01s
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
01:18:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.973 km
Perigee altitude
497.627 km
Semi-major axis
6,881.437 km
Eccentricity
0.00082
Inclination
52.9709°
RAAN
51.7583°
Arg. of periapsis
311.6703°
True anomaly
48.42915°
Mean anomaly
48.3585°
Eccentric anomaly
48.39382°
Mean motion
3.80211 °/min
Orbital period
94.68 mins
BSTAR
0.00042732
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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 | 2025-12-21 06:53:10.872Z | 237.429° WSW | 2025-12-21 06:55:10.872Z | 279.1° WNW | 43.699° | 2025-12-21 06:59:10.872Z | 47.912° ENE |
| 4 mins | 2025-12-21 08:33:10.872Z | 314.465° NW | 2025-12-21 08:34:10.872Z | 333.682° NNW | 17.335° | 2025-12-21 08:37:10.872Z | 24.993° NE |
| 4 mins | 2025-12-21 11:52:10.872Z | 345.78° N | 2025-12-21 11:54:10.872Z | 25.515° NE | 19.428° | 2025-12-21 11:56:10.872Z | 63.071° ENE |
| 6 mins | 2025-12-21 13:30:10.872Z | 307.737° NW | 2025-12-21 13:33:10.872Z | 167.046° S | 44.463° | 2025-12-21 13:36:10.872Z | 133.746° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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