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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 VANGUARD DEB
1 01576U 58002C   25258.39503234  .00000959  00000-0  82994-3 0  9993
2 01576  34.2301  34.0908 1399117 351.2259   6.6079 11.82003934769579
Epoch: 2025-09-15T09:28Z
TLE epoch observation values (Epoch: 2025-09-15T09:28:50.794Z)
Latitude
-0°
Longitude
-102.72115°
Altitude
632.899 km
Speed
8.048 km/s
True Right ascension
02h 16m 21s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
05:17:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,904.761 km
Perigee altitude
626.013 km
Semi-major axis
8,143.524 km
Eccentricity
0.13991
Inclination
34.2301°
RAAN
34.0908°
Arg. of periapsis
351.2259°
True anomaly
8.83613°
Mean anomaly
6.6079°
Eccentric anomaly
7.67908°
Mean motion
2.95342 °/min
Orbital period
121.89 mins
BSTAR
0.00082994
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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