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: 10 hours ago
TLE from 10 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 25329.25653976 .00003960 00000-0 19097-3 0 9993
2 61045 52.9769 167.5123 0009118 222.0778 137.9517 15.20958216 66732Epoch: 2025-11-25T06:09Z
TLE epoch observation values (Epoch: 2025-11-25T06:09:25.035Z)
Latitude
-0°
Longitude
10.71322°
Altitude
508.487 km
Speed
7.608 km/s
True Right ascension
11h 10m 02s
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
13:48:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.508 km
Perigee altitude
496.959 km
Semi-major axis
6,881.371 km
Eccentricity
0.00091
Inclination
52.9769°
RAAN
167.5123°
Arg. of periapsis
222.0778°
True anomaly
138.02162°
Mean anomaly
137.9517°
Eccentric anomaly
137.98667°
Mean motion
3.80216 °/min
Orbital period
94.68 mins
BSTAR
0.00019097
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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 | 2025-11-25 17:25:29.057Z | 272.544° WNW | 2025-11-25 17:28:29.057Z | 323.787° NNW | 24.591° | 2025-11-25 17:31:29.057Z | 26.728° NE |
| 5 mins | 2025-11-25 22:25:29.057Z | 330.259° NNW | 2025-11-25 22:27:29.057Z | 29.186° NE | 36.153° | 2025-11-25 22:30:29.057Z | 105.401° ESE |
| 4 mins | 2025-11-26 00:04:29.057Z | 261.335° W | 2025-11-26 00:05:29.057Z | 240.351° WSW | 20.351° | 2025-11-26 00:08:29.057Z | 182.832° SSW |
| 5 mins | 2025-11-26 15:27:29.057Z | 199.383° SSW | 2025-11-26 15:29:29.057Z | 135.601° SSE | 37.236° | 2025-11-26 15:32:29.057Z | 63.307° ENE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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