VANGUARD DEB, 69999

Orbit data source: Space-Track

VANGUARD DEB, 69999 is space debris in LEO originally from a launch on Mon, 17 Mar 1958 UTC launched from the Air Force Eastern Test Range (AFETR). 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
69999, 1958-002D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1958-03-17 (69 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago
0 VANGUARD DEB
1 69999U 58002D   26300.72124423  .00000126  00000-0  10584-3 0  9993
2 69999  34.2447 309.9338 1478305 232.6785 112.9893 11.62356361202229
Epoch: 2026-10-27T17:18Z
TLE epoch observation values (Epoch: 2026-10-27T17:18:35.501Z)
Latitude
0.00002°
Longitude
14.20559°
Altitude
2,466.766 km
Speed
6.461 km/s
True Right ascension
20h 39m 44s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
06:01:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,074.222 km
Perigee altitude
639.46 km
Semi-major axis
8,234.978 km
Eccentricity
0.14783
Inclination
34.2447°
RAAN
309.9338°
Arg. of periapsis
232.6785°
True anomaly
127.3806°
Mean anomaly
112.9893°
Eccentric anomaly
120.30215°
Mean motion
2.90435 °/min
Orbital period
123.95 mins
BSTAR
0.00010584
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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