SPACEMOBILE-005, 61046
Orbit data source: Space-Track
SPACEMOBILE-005, 61046 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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61046 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: 2 days ago
TLE from 2 days ago
0 SPACEMOBILE-005
1 61046U 24163B 26005.63704968 .00026654 00000-0 11945-2 0 9994
2 61046 52.9722 337.0587 0010722 2.3152 357.7891 15.21028256 73028Epoch: 2026-01-05T15:17Z
TLE epoch observation values (Epoch: 2026-01-05T15:17:21.092Z)
Latitude
0.00006°
Longitude
2.48951°
Altitude
496.242 km
Speed
7.622 km/s
True Right ascension
22h 28m 14s
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
08:00:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.401 km
Perigee altitude
495.645 km
Semi-major axis
6,881.16 km
Eccentricity
0.00107
Inclination
52.9722°
RAAN
337.0587°
Arg. of periapsis
2.3152°
True anomaly
357.78435°
Mean anomaly
357.7891°
Eccentric anomaly
357.78673°
Mean motion
3.80234 °/min
Orbital period
94.68 mins
BSTAR
0.0011945
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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-005 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 | 2026-01-08 00:15:05.842Z | 235.314° WSW | 2026-01-08 00:18:05.842Z | 17.055° NNE | 43.275° | 2026-01-08 00:21:05.842Z | 47.739° ENE |
| 4 mins | 2026-01-08 05:15:05.842Z | 356.562° N | 2026-01-08 05:16:05.842Z | 17.313° NNE | 19.002° | 2026-01-08 05:19:05.842Z | 70.409° E |
| 6 mins | 2026-01-08 06:53:05.842Z | 307.907° NW | 2026-01-08 06:55:05.842Z | 281.449° WNW | 44.62° | 2026-01-08 06:59:05.842Z | 132.617° SE |
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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