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: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 25308.16369736 .00005814 00000-0 27335-3 0 9992
2 61045 52.9764 264.5209 0010669 155.7463 204.4036 15.20956452 63526Epoch: 2025-11-04T03:55Z
TLE epoch observation values (Epoch: 2025-11-04T03:55:43.451Z)
Latitude
-0.00001°
Longitude
161.93519°
Altitude
510.517 km
Speed
7.606 km/s
True Right ascension
17h 38m 05s
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
11:02:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.581 km
Perigee altitude
495.898 km
Semi-major axis
6,881.376 km
Eccentricity
0.00107
Inclination
52.9764°
RAAN
264.5209°
Arg. of periapsis
155.7463°
True anomaly
204.35315°
Mean anomaly
204.4036°
Eccentric anomaly
204.37837°
Mean motion
3.80216 °/min
Orbital period
94.68 mins
BSTAR
0.00027335
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-04 23:00:37.987Z | 180.436° SSW | 2025-11-04 23:02:37.987Z | 143.817° SSE | 22.797° | 2025-11-04 23:05:37.987Z | 80.514° E |
| 5 mins | 2025-11-05 00:39:37.987Z | 269.625° W | 2025-11-05 00:41:37.987Z | 332.269° NNW | 33.615° | 2025-11-05 00:44:37.987Z | 36.111° NE |
| 5 mins | 2025-11-05 05:38:37.987Z | 346.003° N | 2025-11-05 05:40:37.987Z | 39.263° NE | 25.901° | 2025-11-05 05:43:37.987Z | 91.216° ESE |
| 5 mins | 2025-11-05 07:16:37.987Z | 287.039° WNW | 2025-11-05 07:18:37.987Z | 238.399° WSW | 32.647° | 2025-11-05 07:21:37.987Z | 160.963° S |
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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