Showing default

CELESTIS 17/SHERPA-FX1, 47486

Orbit data source: Space-Track

CELESTIS 17/SHERPA-FX1, 47486 is a payload satellite owned by Spaceflight Ind (US) in SSO that was launched on Sun, 24 Jan 2021 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
47486, 2021-006CB
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spaceflight Ind
Mission
Operational Commercial Technology
Bus & Motor
ESPA/SHERPA-FX, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
2021-01-24 (5 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.4 m
Radar Cross Section
0.503 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 CELESTIS 17/SHERPA-FX1
1 47486U 21006CB  26082.36774133  .00007289  00000-0  24428-3 0  9999
2 47486  97.2369 125.5012 0007972 134.6698 225.5194 15.31178983286162
Epoch: 2026-03-23T08:49Z
TLE epoch observation values (Epoch: 2026-03-23T08:49:32.850Z)
Latitude
-0.00011°
Longitude
172.25358°
Altitude
479.233 km
Speed
7.624 km/s
True Right ascension
08h 22m 00s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
22:38:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.696 km
Perigee altitude
463.779 km
Semi-major axis
6,847.374 km
Eccentricity
0.0008
Inclination
97.2369°
RAAN
125.5012°
Arg. of periapsis
134.6698°
True anomaly
225.45427°
Mean anomaly
225.5194°
Eccentric anomaly
225.48683°
Mean motion
3.83051 °/min
Orbital period
93.98 mins
BSTAR
0.00024428
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|