Showing default

ERS 6, 608

Orbit data source: Space-Track

ERS 6, 608 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Thu, 09 May 1963 UTC via an ATLAS AGENA B 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
608, 1963-014C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
TRW
Mission
Defense Technology
Bus & Motor
TRS, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
1963-05-09 (62 years ago)
Launch vehicle
ATLAS AGENA B
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box, 0.1 m
Radar Cross Section
0.032 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 ERS 6
1 00608U 63014C   25257.27199205  .00000055  00000-0  24546-1 0  9996
2 00608  87.3364 219.4420 0043296 289.1139  70.5031  8.65285237969631
Epoch: 2025-09-14T06:31Z
TLE epoch observation values (Epoch: 2025-09-14T06:31:40.113Z)
Latitude
0.00003°
Longitude
128.03148°
Altitude
3,631.916 km
Speed
6.316 km/s
True Right ascension
14h 37m 46s
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
11:12:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,685.252 km
Perigee altitude
3,598.486 km
Semi-major axis
10,020.006 km
Eccentricity
0.00433
Inclination
87.3364°
RAAN
219.442°
Arg. of periapsis
289.1139°
True anomaly
70.97163°
Mean anomaly
70.5031°
Eccentric anomaly
70.73728°
Mean motion
2.16392 °/min
Orbital period
166.36 mins
BSTAR
0.024546
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|