Showing default

RIDESHARE ADAPTER, 47435

Orbit data source: Space-Track

RIDESHARE ADAPTER, 47435 is a payload satellite owned by SpaceX (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
47435, 2021-006Y
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
SpaceX
Mission
Non-operational Commercial Technology
Bus & Motor
ESPA, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
2021-01-24 (6 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.0 m
Radar Cross Section
11.058 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 RIDESHARE ADAPTER
1 47435U 21006Y   26207.62834418  .00015752  00000-0  31086-3 0  9996
2 47435  97.2188 261.5223 0007121  32.4216 327.7471 15.47226610306240
Epoch: 2026-07-26T15:04Z
TLE epoch observation values (Epoch: 2026-07-26T15:04:48.937Z)
Latitude
0.00004°
Longitude
90.99485°
Altitude
423.879 km
Speed
7.659 km/s
True Right ascension
17h 26m 05s
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
15:53:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
426.607 km
Perigee altitude
416.923 km
Semi-major axis
6,799.902 km
Eccentricity
0.00071
Inclination
97.2188°
RAAN
261.5223°
Arg. of periapsis
32.4216°
True anomaly
327.70352°
Mean anomaly
327.7471°
Eccentric anomaly
327.72531°
Mean motion
3.8707 °/min
Orbital period
93.01 mins
BSTAR
0.00031086
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|