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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: 5 hours ago

TLE from 5 hours ago
0 SECOR 3
1 01208U 65016E   26038.32793587  .00000070  00000-0  89434-4 0  9991
2 01208  70.0789 100.6890 0023045 257.8858 178.5044 13.96057769101043
Epoch: 2026-02-07T07:52Z
TLE epoch observation values (Epoch: 2026-02-07T07:52:13.659Z)
Latitude
66.13673°
Longitude
-100.23676°
Altitude
935.092 km
Speed
7.382 km/s
True Right ascension
10h 21m 05s
True Declination
66° 00' 44"
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
14:56:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
922.299 km
Perigee altitude
888.728 km
Semi-major axis
7,283.651 km
Eccentricity
0.0023
Inclination
70.0789°
RAAN
100.689°
Arg. of periapsis
257.8858°
True anomaly
178.51127°
Mean anomaly
178.5044°
Eccentric anomaly
178.50784°
Mean motion
3.49156 °/min
Orbital period
103.11 mins
BSTAR
0.000089434
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