Showing default

ORS 5 SENSORSAT, 42921

Orbit data source: Space-Track

ORS 5 SENSORSAT, 42921 is a payload satellite owned by DoD ORS (US) in LEO that was launched on Sat, 26 Aug 2017 UTC via an MINOTAUR IV 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.

Not visible in the next 10 days
Identifier
42921, 2017-050A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
MIT-LL
Mission
Operational Defense Early Warn
Bus & Motor
ORS-5, Unknown motor
Mass
~110 kg wet, ~110 kg dry
Launch date (UTC)
2017-08-26 (8 years ago)
Launch vehicle
MINOTAUR IV
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
1.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ORS 5 SENSORSAT
1 42921U 17050A   25259.95630585  .00003066  00000-0  17792-3 0  9999
2 42921   0.0498  20.0931 0010698 312.0730  27.7768 14.99400041439999
Epoch: 2025-09-16T22:57Z
TLE epoch observation values (Epoch: 2025-09-16T22:57:04.825Z)
Latitude
-0.0172°
Longitude
19.5907°
Altitude
559.026 km
Speed
7.589 km/s
True Right ascension
23h 59m 59s
True Declination
0° 01' 02"
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
00:21:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.536 km
Perigee altitude
567.659 km
Semi-major axis
6,953.234 km
Eccentricity
0.00107
Inclination
0.0498°
RAAN
20.0931°
Arg. of periapsis
312.073°
True anomaly
27.834°
Mean anomaly
27.7768°
Eccentric anomaly
27.80539°
Mean motion
3.74337 °/min
Orbital period
96.17 mins
BSTAR
0.00017792
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
|