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: 22 hours ago
TLE from 22 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 26062.35501045 .00002712 00000-0 13438-3 0 9995
2 61045 52.9675 76.2279 0007090 166.6433 193.4751 15.21236864 81669Epoch: 2026-03-03T08:31Z
TLE epoch observation values (Epoch: 2026-03-03T08:31:12.902Z)
Latitude
0.00002°
Longitude
147.28889°
Altitude
507.728 km
Speed
7.609 km/s
True Right ascension
05h 04m 54s
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
10:05:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.273 km
Perigee altitude
497.517 km
Semi-major axis
6,880.532 km
Eccentricity
0.00071
Inclination
52.9675°
RAAN
76.2279°
Arg. of periapsis
166.6433°
True anomaly
193.45618°
Mean anomaly
193.4751°
Eccentric anomaly
193.46564°
Mean motion
3.80286 °/min
Orbital period
94.67 mins
BSTAR
0.00013438
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-04 08:37:37.055Z | 352.267° N | 2026-03-04 08:38:37.055Z | 11.473° NNE | 17.769° | 2026-03-04 08:41:37.055Z | 65.657° ENE |
| 6 mins | 2026-03-04 10:15:37.055Z | 311.364° NW | 2026-03-04 10:17:37.055Z | 320.901° NNW | 42.925° | 2026-03-04 10:21:37.055Z | 128.945° SE |
| 5 mins | 2026-03-05 03:17:37.055Z | 232.234° WSW | 2026-03-05 03:19:37.055Z | 274.887° WNW | 44.839° | 2026-03-05 03:22:37.055Z | 49.068° ENE |
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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