ATLAS CENTAUR 2 DEB, 19638
Orbit data source: Space-Track
ATLAS CENTAUR 2 DEB, 19638 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 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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19638 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
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 ATLAS CENTAUR 2 DEB
1 19638U 63047S 26125.09847747 -.00003091 00000-0 -91008-2 0 9994
2 19638 31.0035 55.4794 0625497 346.1046 132.8886 12.55674024569239Epoch: 2026-05-05T02:21Z
TLE epoch observation values (Epoch: 2026-05-05T02:21:48.453Z)
Latitude
25.38354°
Longitude
-74.75111°
Altitude
1,787.916 km
Speed
6.834 km/s
True Right ascension
12h 14m 42s
True Declination
25° 16' 03"
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
05:38:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,933.557 km
Perigee altitude
954.979 km
Semi-major axis
7,822.405 km
Eccentricity
0.06255
Inclination
31.0035°
RAAN
55.4794°
Arg. of periapsis
346.1046°
True anomaly
137.86814°
Mean anomaly
132.8886°
Eccentric anomaly
135.40479°
Mean motion
3.13713 °/min
Orbital period
114.75 mins
BSTAR
-0.0091008
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Other satellites on launch #47 in the year 1963 (1963-11-27 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.ATLAS CENTAUR 2 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-05-05 22:55:15.366Z | 213.372° SW | 2026-05-05 23:01:15.366Z | 156.309° SSE | 26.284° | 2026-05-05 23:08:15.366Z | 101.022° ESE |
| 15 mins | 2026-05-06 00:57:15.366Z | 237.534° WSW | 2026-05-06 01:03:15.366Z | 166.552° S | 36.262° | 2026-05-06 01:12:15.366Z | 104.376° ESE |
| 17 mins | 2026-05-06 02:58:15.366Z | 254.076° W | 2026-05-06 03:05:15.366Z | 189.272° SSW | 35.053° | 2026-05-06 03:15:15.366Z | 123.961° SE |
| 15 mins | 2026-05-06 05:01:15.366Z | 249.933° W | 2026-05-06 05:07:15.366Z | 207.969° SW | 24.507° | 2026-05-06 05:16:15.366Z | 155.23° 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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