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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-003
1 61045U 24163A 26259.37520582 .00000856 00000-0 53523-4 0 9999
2 61045 52.9651 250.1683 0006332 36.4080 323.7343 15.20425662111647Epoch: 2026-09-16T09:00Z
TLE epoch observation values (Epoch: 2026-09-16T09:00:17.782Z)
Latitude
-0.00009°
Longitude
119.76644°
Altitude
501.918 km
Speed
7.617 km/s
True Right ascension
16h 40m 40s
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
03:01:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.201 km
Perigee altitude
500.484 km
Semi-major axis
6,882.979 km
Eccentricity
0.00063
Inclination
52.9651°
RAAN
250.1683°
Arg. of periapsis
36.408°
True anomaly
323.69135°
Mean anomaly
323.7343°
Eccentric anomaly
323.71283°
Mean motion
3.80083 °/min
Orbital period
94.72 mins
BSTAR
0.000053523
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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 | 2026-09-18 00:35:52.521Z | 161.752° S | 2026-09-18 00:37:52.521Z | 127.602° SE | 16.342° | 2026-09-18 00:39:52.521Z | 93.272° ESE |
| 6 mins | 2026-09-18 02:13:52.521Z | 247.709° W | 2026-09-18 02:15:52.521Z | 303.164° NW | 60.584° | 2026-09-18 02:19:52.521Z | 44.723° NE |
| 5 mins | 2026-09-18 07:12:52.521Z | 343.214° N | 2026-09-18 07:14:52.521Z | 23.809° NE | 22.883° | 2026-09-18 07:17:52.521Z | 77.168° E |
| 5 mins | 2026-09-18 08:51:52.521Z | 298.559° NW | 2026-09-18 08:53:52.521Z | 211.861° SW | 67.374° | 2026-09-18 08:56:52.521Z | 141.607° SSE |
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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