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: 15 hours ago

TLE from 15 hours ago
0 VANGUARD DEB
1 01576U 58002C   25309.76281891  .00000479  00000-0  40325-3 0  9992
2 01576  34.2333 206.3924 1395711 265.4089  78.6273 11.82107580775652
Epoch: 2025-11-05T18:18Z
TLE epoch observation values (Epoch: 2025-11-05T18:18:27.553Z)
Latitude
-0.00006°
Longitude
-113.45332°
Altitude
1,693.776 km
Speed
7.059 km/s
True Right ascension
13h 45m 34s
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
05:12:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,901.444 km
Perigee altitude
628.376 km
Semi-major axis
8,143.047 km
Eccentricity
0.13957
Inclination
34.2333°
RAAN
206.3924°
Arg. of periapsis
265.4089°
True anomaly
94.65242°
Mean anomaly
78.6273°
Eccentric anomaly
86.61014°
Mean motion
2.95368 °/min
Orbital period
121.88 mins
BSTAR
0.00040325
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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