Showing default

PROPCUBE 3, 40973

Orbit data source: Space-Track

PROPCUBE 3, 40973 is a payload satellite owned by USN PGS (US) in LEO that was launched on Thu, 08 Oct 2015 UTC via an ATLAS V 401 launch vehicle from the Air Force Western Test Range (AFWTR). 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
40973, 2015-058K
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Tyvak NSS
Mission
Operational Defense Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2015-10-08 (10 years ago)
Launch vehicle
ATLAS V 401
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 PROPCUBE 3
1 40973U 15058K   26037.19023633  .00005671  00000-0  47788-3 0  9993
2 40973  64.7698 301.5070 0125490 112.2251 249.2230 14.93208459 95232
Epoch: 2026-02-06T04:33Z
TLE epoch observation values (Epoch: 2026-02-06T04:33:56.418Z)
Latitude
-0.00004°
Longitude
96.69024°
Altitude
621.915 km
Speed
7.531 km/s
True Right ascension
20h 06m 01s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
16:22:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
673.904 km
Perigee altitude
499.106 km
Semi-major axis
6,964.642 km
Eccentricity
0.01255
Inclination
64.7698°
RAAN
301.507°
Arg. of periapsis
112.2251°
True anomaly
247.88607°
Mean anomaly
249.223°
Eccentric anomaly
248.55378°
Mean motion
3.73418 °/min
Orbital period
96.41 mins
BSTAR
0.00047788
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
|