SCOUT A R/B, 2755

Orbit data source: Space-Track

SCOUT A R/B, 2755 is space debris in LEO originally from a launch on Fri, 14 Apr 1967 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
2755, 1967-034B
Orbit
LEO
Last TLE update
15 hours ago
Origin
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1967-04-14 (58 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 15 hours ago
0 SCOUT A R/B
1 02755U 67034B   25199.85717426 -.00000035  00000-0 -64063-4 0  9998
2 02755  90.2555  47.1437 0023885 240.5987 130.4653 13.53973407876931
Epoch: 2025-07-18T20:34Z
TLE epoch observation values (Epoch: 2025-07-18T20:34:19.856Z)
Latitude
11.22358°
Longitude
161.60791°
Altitude
1,071.433 km
Speed
7.311 km/s
True Right ascension
03h 08m 22s
True Declination
11° 09' 39"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
57.7343°
Longitude
-17.9231°
Altitude
1,075.35 km
Speed
7.316 km/s
Apparent Right ascension
13h 29m 22s
Apparent Declination
15° 04' 13"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:08:11
Azimuth
336.779° NNW
Elevation
-31.857°
Doppler factor
1
Orbital elements
Apogee altitude
1,072.473 km
Perigee altitude
1,036.966 km
Semi-major axis
7,432.856 km
Eccentricity
0.00239
Inclination
90.2555°
RAAN
47.1437°
Arg. of periapsis
240.5987°
True anomaly
130.67313°
Mean anomaly
130.4653°
Eccentric anomaly
130.56925°
Mean motion
3.38696 °/min
Orbital period
106.29 mins
BSTAR
-0.000064063
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