Showing default

APRIZESAT 10, 40019

Orbit data source: Space-Track

APRIZESAT 10, 40019 is a payload satellite owned by SpaceQuest (US) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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
40019, 2014-033K
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
SpaceQuest
Mission
Operational Commercial Communications
Bus & Motor
APRIZE, Unknown motor
Mass
14 kg wet, 14 kg dry
Launch date (UTC)
2014-06-19 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Ant, 0.1 m
Radar Cross Section
0.060 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 APRIZESAT 10
1 40019U 14033K   26123.84051245  .00000538  00000-0  91890-4 0  9995
2 40019  97.9584 251.8067 0079950  56.0321 304.8451 14.70843853635736
Epoch: 2026-05-03T20:10Z
TLE epoch observation values (Epoch: 2026-05-03T20:10:20.275Z)
Latitude
-0.00002°
Longitude
87.48394°
Altitude
629.538 km
Speed
7.561 km/s
True Right ascension
16h 47m 13s
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
21:14:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
711.664 km
Perigee altitude
599.198 km
Semi-major axis
7,033.568 km
Eccentricity
0.008
Inclination
97.9584°
RAAN
251.8067°
Arg. of periapsis
56.0321°
True anomaly
304.08891°
Mean anomaly
304.8451°
Eccentric anomaly
304.46744°
Mean motion
3.67942 °/min
Orbital period
97.84 mins
BSTAR
0.00009189
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
|