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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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 26139.56394066 -.00048934 00000-0 -21962-2 0 9994
2 61045 52.9643 81.0741 0007012 32.4276 327.7148 15.20706493 93418Epoch: 2026-05-19T13:32Z
TLE epoch observation values (Epoch: 2026-05-19T13:32:04.473Z)
Latitude
0.00002°
Longitude
0.81944°
Altitude
500.505 km
Speed
7.618 km/s
True Right ascension
05h 24m 17s
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
14:21:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.821 km
Perigee altitude
499.169 km
Semi-major axis
6,882.132 km
Eccentricity
0.0007
Inclination
52.9643°
RAAN
81.0741°
Arg. of periapsis
32.4276°
True anomaly
327.67185°
Mean anomaly
327.7148°
Eccentric anomaly
327.69333°
Mean motion
3.80153 °/min
Orbital period
94.7 mins
BSTAR
-0.0021962
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-20 05:48:42.386Z | 306.648° NW | 2026-05-20 05:51:42.386Z | 270.254° WNW | 43.531° | 2026-05-20 05:55:42.386Z | 135.734° SSE |
| 6 mins | 2026-05-20 22:51:42.386Z | 241.49° WSW | 2026-05-20 22:53:42.386Z | 278.259° WNW | 41.624° | 2026-05-20 22:57:42.386Z | 46.123° ENE |
| 4 mins | 2026-05-21 00:31:42.386Z | 312.312° NW | 2026-05-21 00:33:42.386Z | 350.373° N | 16.312° | 2026-05-21 00:35:42.386Z | 22.562° NE |
| 4 mins | 2026-05-21 03:51:42.386Z | 358.479° N | 2026-05-21 03:52:42.386Z | 20.533° NNE | 20.171° | 2026-05-21 03:55:42.386Z | 74.127° E |
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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