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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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: 23 hours ago
TLE from 23 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 26199.28569049 .00002152 00000-0 11126-3 0 9997
2 61046 52.9757 166.3840 0008561 205.2960 154.7616 15.20722937102490Epoch: 2026-07-18T06:51Z
TLE epoch observation values (Epoch: 2026-07-18T06:51:23.658Z)
Latitude
-0.00002°
Longitude
127.43478°
Altitude
509.865 km
Speed
7.607 km/s
True Right ascension
11h 05m 32s
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
18:59:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.836 km
Perigee altitude
498.052 km
Semi-major axis
6,882.081 km
Eccentricity
0.00086
Inclination
52.9757°
RAAN
166.384°
Arg. of periapsis
205.296°
True anomaly
154.80339°
Mean anomaly
154.7616°
Eccentric anomaly
154.7825°
Mean motion
3.80157 °/min
Orbital period
94.7 mins
BSTAR
0.00011126
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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 | 2026-07-19 07:00:36.745Z | 318.369° NNW | 2026-07-19 07:03:36.745Z | 48.994° ENE | 41.166° | 2026-07-19 07:06:36.745Z | 116.443° SE |
| 5 mins | 2026-07-20 00:03:36.745Z | 213.596° SW | 2026-07-20 00:05:36.745Z | 123.607° SE | 42.762° | 2026-07-20 00:08:36.745Z | 56.311° ENE |
| 4 mins | 2026-07-20 01:42:36.745Z | 298.344° NW | 2026-07-20 01:44:36.745Z | 341.589° N | 21.123° | 2026-07-20 01:46:36.745Z | 19.865° NNE |
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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