Showing default

SPACEMOBILE-001, 61047

Orbit data source: Space-Track

SPACEMOBILE-001, 61047 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.

Loading next visibility...
Identifier
61047, 2024-163C
Orbit
LEO
Last TLE update
13 hours ago
Origin
Manufacturer
AST & Science
Mission
Operational Commercial Communications
Bus & Motor
BW3, Unknown motor
Mass
1,500 kg wet, 1,500 kg dry
Launch date (UTC)
2024-09-12 (8 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Plate, 9 m
Radar Cross Section
1.500 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 13 hours ago
0 SPACEMOBILE-001
1 61047U 24163C   25133.89765551  .00002002  00000-0  10622-3 0  9992
2 61047  52.9722 345.3044 0010174   0.7085 359.3921 15.20142471 37002
Epoch: 2025-05-13T21:32Z
Definitive object data (Epoch: 2025-05-13T21:32:37.436Z)
Latitude
-0.00005°
Longitude
150.25859°
Altitude
499.283 km
Speed
7.62 km/s
True Right ascension
23h 01m 13s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
35.51561°
Longitude
-179.82693°
Altitude
503.035 km
Speed
7.62 km/s
Apparent Right ascension
03h 41m 20s
Apparent Declination
0° 42' 33"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
18:51:23
Azimuth
60.111° ENE
Elevation
-31.73°
Doppler factor
1
Orbital elements
Apogee altitude
512.7 km
Perigee altitude
498.692 km
Semi-major axis
6,883.833 km
Eccentricity
0.0010174
Inclination
52.9722°
RAAN
345.3044°
Arg. of periapsis
0.7085°
True anomaly
359.39086°
Mean anomaly
359.3921°
Eccentric anomaly
359.39148°
Mean motion
3.80012 °/min
BSTAR
0.00010622
Orbital period
94.73 mins
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

SPACEMOBILE-001 Visibility forecast

Observer location: undefined°, undefined°

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 mins2025-05-14 16:39:12.295Z221.676° SW2025-05-14 16:42:12.295Z159.275° S43.651°2025-05-14 16:45:12.295Z55.132° ENE
4 mins2025-05-14 18:20:12.295Z312.377° NW2025-05-14 18:21:12.295Z334.82° NNW20.309°2025-05-14 18:24:12.295Z27.648° NE
5 mins2025-05-14 23:18:12.295Z320.684° NNW2025-05-14 23:20:12.295Z51.257° ENE42.911°2025-05-14 23:23:12.295Z120.312° SE
|