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SECOR 8 (EGRS 8), 2520

Orbit data source: Space-Track

SECOR 8 (EGRS 8), 2520 is an American payload satellite in LEO that was launched on Wed, 05 Oct 1966 UTC via an ATLAS SLV-3 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
2520, 1966-089B
Orbit
LEO
Last TLE update
2 days ago
Origin
Manufacturer
ITT
Mission
Defense Geodetic
Bus & Motor
SECOR, Unknown motor
Mass
18 kg wet, 18 kg dry
Launch date (UTC)
1966-10-05 (59 years ago)
Launch vehicle
ATLAS SLV-3 AGENA D
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.36 m
Radar Cross Section
0.095 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 days ago
0 SECOR 8 (EGRS 8)
1  2520U 66089B   25127.17202995 -.00000000  00000-0 -10579-2 0  9996
2  2520  89.8285  33.8887 0014993 357.2250   2.8516  8.58894638839672
Epoch: 2025-05-07T04:07Z
Definitive object data (Epoch: 2025-05-07T04:07:43.387Z)
Latitude
-0.00003°
Longitude
106.69722°
Altitude
3,680.799 km
Speed
6.3 km/s
True Right ascension
02h 15m 33s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
-16.17679°
Longitude
106.63507°
Altitude
3,684.623 km
Speed
6.299 km/s
Apparent Right ascension
02h 19m 31s
Apparent Declination
-25° 14' 15"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
14:27:51
Azimuth
7.407° NNE
Elevation
-75.218°
Doppler factor
1
Orbital elements
Apogee altitude
3,706.615 km
Perigee altitude
3,676.42 km
Semi-major axis
10,069.655 km
Eccentricity
0.0014993
Inclination
89.8285°
RAAN
33.8887°
Arg. of periapsis
357.225°
True anomaly
2.86016°
Mean anomaly
2.8516°
Eccentric anomaly
2.85588°
Mean motion
2.14794 °/min
BSTAR
-0.0010579
Orbital period
167.6 mins
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Other satellites on launch #89 in the year 1966 (1966-10-05 UTC)

SECOR 8 (EGRS 8) Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
34 mins2025-05-09 07:13:03.051Z355.331° N2025-05-09 07:30:03.051Z289.688° WNW37.398°2025-05-09 07:47:03.051Z221.228° SW
22 mins2025-05-09 15:03:03.051Z92.042° ESE2025-05-09 15:13:03.051Z56.146° ENE20.849°2025-05-09 15:25:03.051Z13.922° NNE
37 mins2025-05-09 17:38:03.051Z169.297° S2025-05-09 17:56:03.051Z78.251° E44.893°2025-05-09 18:15:03.051Z359.65° N
27 mins2025-05-09 20:33:03.051Z245.579° WSW2025-05-09 20:46:03.051Z293.594° NW23.05°2025-05-09 21:00:03.051Z344.369° N
24 mins2025-05-10 02:51:03.051Z21.925° NNE2025-05-10 03:02:03.051Z61.106° ENE19.51°2025-05-10 03:15:03.051Z106.597° ESE
36 mins2025-05-10 05:36:03.051Z2.186° NNE2025-05-10 05:53:03.051Z65.345° ENE44.882°2025-05-10 06:12:03.051Z183.625° SSW
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