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SECOR 3, 1208

Orbit data source: Space-Track

SECOR 3, 1208 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D 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.

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Identifier
1208, 1965-016E
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ITT
Mission
Spacecraft
Bus & Motor
SECOR, Unknown motor
Mass
18 kg wet, 18 kg dry
Launch date (UTC)
1965-03-09 (61 years ago)
Launch vehicle
THOR SLV-2 AGENA D
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 SECOR 3
1 01208U 65016E   25293.91515103  .00000116  00000-0  12271-3 0  9999
2 01208  70.0804 333.7140 0018467  32.9676  25.4274 13.96027858 85772
Epoch: 2025-10-20T21:57Z
TLE epoch observation values (Epoch: 2025-10-20T21:57:49.048Z)
Latitude
53.38655°
Longitude
3.6713°
Altitude
903.565 km
Speed
7.412 km/s
True Right ascension
00h 10m 56s
True Declination
53° 13' 30"
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
13:44:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
919.068 km
Perigee altitude
892.167 km
Semi-major axis
7,283.754 km
Eccentricity
0.00185
Inclination
70.0804°
RAAN
333.714°
Arg. of periapsis
32.9676°
True anomaly
25.51845°
Mean anomaly
25.4274°
Eccentric anomaly
25.47291°
Mean motion
3.49149 °/min
Orbital period
103.11 mins
BSTAR
0.00012271
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