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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: 8 hours ago

TLE from 8 hours ago
0 SECOR 3
1  1208U 65016E   25343.15025264  .00000098  00000-0  10938-3 0  9992
2  1208  70.0791 228.8526 0021512 328.4059 147.3602 13.96042359 92648
Epoch: 2025-12-09T03:36Z
TLE epoch observation values (Epoch: 2025-12-09T03:36:21.828Z)
Latitude
57.86226°
Longitude
-118.39783°
Altitude
929.88 km
Speed
7.386 km/s
True Right ascension
00h 55m 19s
True Declination
57° 42' 39"
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
10:18:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
921.236 km
Perigee altitude
889.898 km
Semi-major axis
7,283.704 km
Eccentricity
0.00215
Inclination
70.0791°
RAAN
228.8526°
Arg. of periapsis
328.4059°
True anomaly
147.49286°
Mean anomaly
147.3602°
Eccentric anomaly
147.42656°
Mean motion
3.49152 °/min
Orbital period
103.11 mins
BSTAR
0.00010938
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