Showing default

NAVSTAR 70 (USA 251), 39741

Orbit data source: Space-Track

NAVSTAR 70 (USA 251), 39741 is a payload satellite owned by USAF SMC (US) in MEO that was launched on Sat, 17 May 2014 UTC via a DELTA 4M+(4,2) 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
39741, 2014-026A
Orbit
MEO
Country
Flag of USUS
Related business
Manufacturer
Boeing/ES
Mission
Operational Defense Navigation
Bus & Motor
GPS IIF, AOCS
Mass
1,630 kg wet, ~1,500 kg dry
Launch date (UTC)
2014-05-17 (12 years ago)
Launch vehicle
DELTA 4M+(4,2)
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 9.0 m
Radar Cross Section
13.960 m², Large (>1 m²)

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

TLE from 17 hours ago
0 NAVSTAR 70 (USA 251)
1 39741U 14026A   26257.21083856 -.00000095  00000-0  00000-0 0  9997
2 39741  56.4481 328.0490 0039345 324.1570  35.6413  2.00554646 90324
Epoch: 2026-09-14T05:03Z
TLE epoch observation values (Epoch: 2026-09-14T05:03:36.451Z)
Latitude
0.00005°
Longitude
-101.03261°
Altitude
20,098.438 km
Speed
3.886 km/s
True Right ascension
21h 52m 15s
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
14:35:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,287.453 km
Perigee altitude
20,078.444 km
Semi-major axis
26,561.086 km
Eccentricity
0.00393
Inclination
56.4481°
RAAN
328.049°
Arg. of periapsis
324.157°
True anomaly
35.90507°
Mean anomaly
35.6413°
Eccentric anomaly
35.77308°
Mean motion
0.50139 °/min
Orbital period
718.01 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|