VANGUARD DEB, 1576

Orbit data source: Space-Track

VANGUARD DEB, 1576 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
1576, 1958-002C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1958-03-17 (68 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 VANGUARD DEB
1  1576U 58002C   25353.53186245 -.00000140  00000-0 -12020-3 0  9991
2  1576  34.2240  46.4603 1390051 139.0930 232.2780 11.82212181780830
Epoch: 2025-12-19T12:45Z
TLE epoch observation values (Epoch: 2025-12-19T12:45:52.915Z)
Latitude
0.00001°
Longitude
126.61816°
Altitude
2,539.221 km
Speed
6.361 km/s
True Right ascension
03h 05m 50s
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
05:05:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,896.289 km
Perigee altitude
632.572 km
Semi-major axis
8,142.568 km
Eccentricity
0.13901
Inclination
34.224°
RAAN
46.4603°
Arg. of periapsis
139.093°
True anomaly
220.96593°
Mean anomaly
232.278°
Eccentric anomaly
226.50075°
Mean motion
2.95394 °/min
Orbital period
121.87 mins
BSTAR
-0.0001202
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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