SCOUT A DEB, 2702

Orbit data source: Space-Track

SCOUT A DEB, 2702 is space debris in LEO originally from a launch on Thu, 18 Aug 1966 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
2702, 1966-076D
Orbit
LEO
Last TLE update
16 hours ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1966-08-18 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 16 hours ago
0 SCOUT A DEB
1 02702U 66076D   25199.28976375  .00000019  00000-0  99540-5 0  9991
2 02702  88.5684 305.1550 0090806 135.1662 255.4170 13.36482964851732
Epoch: 2025-07-18T06:57Z
TLE epoch observation values (Epoch: 2025-07-18T06:57:15.588Z)
Latitude
29.61436°
Longitude
-94.69351°
Altitude
1,143.872 km
Speed
7.275 km/s
True Right ascension
20h 23m 51s
True Declination
29° 28' 28"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
86.17906°
Longitude
-73.74409°
Altitude
1,089.283 km
Speed
7.337 km/s
Apparent Right ascension
23h 59m 23s
Apparent Declination
32° 18' 47"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:12:05
Azimuth
2.817° NNE
Elevation
-17.711°
Doppler factor
1
Orbital elements
Apogee altitude
1,187.567 km
Perigee altitude
1,051.401 km
Semi-major axis
7,497.621 km
Eccentricity
0.00908
Inclination
88.5684°
RAAN
305.155°
Arg. of periapsis
135.1662°
True anomaly
254.41288°
Mean anomaly
255.417°
Eccentric anomaly
254.91465°
Mean motion
3.34317 °/min
Orbital period
107.68 mins
BSTAR
0.000009954
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