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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1576 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 VANGUARD DEB
1 01576U 58002C 25339.59299123 .00001472 00000-0 13245-2 0 9997
2 01576 34.2214 97.3907 1391432 64.6618 309.1477 11.82196114779183Epoch: 2025-12-05T14:13Z
TLE epoch observation values (Epoch: 2025-12-05T14:13:54.442Z)
Latitude
-0.00001°
Longitude
169.28099°
Altitude
1,153.441 km
Speed
7.544 km/s
True Right ascension
06h 29m 33s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:10:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,897.498 km
Perigee altitude
631.512 km
Semi-major axis
8,142.642 km
Eccentricity
0.13914
Inclination
34.2214°
RAAN
97.3907°
Arg. of periapsis
64.6618°
True anomaly
295.40041°
Mean anomaly
309.1477°
Eccentric anomaly
302.41777°
Mean motion
2.9539 °/min
Orbital period
121.87 mins
BSTAR
0.0013245
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.VANGUARD DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-06 12:49:14.913Z | 224.882° SW | 2025-12-06 12:52:14.913Z | 165.941° S | 28.709° | 2025-12-06 12:56:14.913Z | 103.286° ESE |
| 8 mins | 2025-12-06 14:57:14.913Z | 247.589° W | 2025-12-06 15:00:14.913Z | 185.964° SSW | 33.946° | 2025-12-06 15:05:14.913Z | 116.218° SE |
| 8 mins | 2025-12-06 17:06:14.913Z | 234.691° WSW | 2025-12-06 17:09:14.913Z | 191.63° SSW | 23.793° | 2025-12-06 17:14:14.913Z | 148.18° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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