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: 12 hours ago

TLE from 12 hours ago
0 CELESTIS 17/SHERPA-FX1
1 47486U 21006CB  25287.84866890  .00007137  00000-0  25882-3 0  9997
2 47486  97.2637 329.8381 0006975   8.1989 351.9364 15.28620071261777
Epoch: 2025-10-14T20:22Z
TLE epoch observation values (Epoch: 2025-10-14T20:22:04.992Z)
Latitude
-0.00004°
Longitude
0.6861°
Altitude
478.305 km
Speed
7.629 km/s
True Right ascension
21h 59m 21s
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
03:23:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.666 km
Perigee altitude
472.103 km
Semi-major axis
6,855.022 km
Eccentricity
0.0007
Inclination
97.2637°
RAAN
329.8381°
Arg. of periapsis
8.1989°
True anomaly
351.92518°
Mean anomaly
351.9364°
Eccentric anomaly
351.93079°
Mean motion
3.82411 °/min
Orbital period
94.14 mins
BSTAR
0.00025882
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|