SCOUT A R/B, 3137

Orbit data source: Space-Track

SCOUT A R/B, 3137 is space debris in LEO originally from a launch on Sat, 02 Mar 1968 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
3137, 1968-012B
Orbit
LEO
Last TLE update
12 hours ago
Origin
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1968-03-02 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 12 hours ago
0 SCOUT A R/B
1 03137U 68012B   25199.47846084  .00000079  00000-0  10915-3 0  9993
2 03137  90.0273 272.6390 0073435 316.9863  42.5562 13.50257011823758
Epoch: 2025-07-18T11:28Z
TLE epoch observation values (Epoch: 2025-07-18T11:28:59.016Z)
Latitude
0.00005°
Longitude
163.86376°
Altitude
1,034.148 km
Speed
7.354 km/s
True Right ascension
18h 10m 33s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
-44.66493°
Longitude
163.89201°
Altitude
1,033.874 km
Speed
7.361 km/s
Apparent Right ascension
21h 11m 16s
Apparent Declination
-53° 22' 16"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
12:30:34
Azimuth
128.953° SE
Elevation
-54.112°
Doppler factor
1
Orbital elements
Apogee altitude
1,123.046 km
Perigee altitude
1,013.679 km
Semi-major axis
7,446.499 km
Eccentricity
0.00734
Inclination
90.0273°
RAAN
272.639°
Arg. of periapsis
316.9863°
True anomaly
43.12918°
Mean anomaly
42.5562°
Eccentric anomaly
42.8423°
Mean motion
3.37765 °/min
Orbital period
106.58 mins
BSTAR
0.00010915
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