OPS 4682 DEB, 19964
Orbit data source: Space-Track
OPS 4682 DEB, 19964 is space debris in LEO originally from a launch on Sat, 03 Apr 1965 UTC launched from the Air Force Western Test Range (AFWTR). 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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19964 intel report (Beta)
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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 OPS 4682 DEB
1 19964U 65027BA 25300.99099899 .00000740 00000-0 25434-2 0 9992
2 19964 90.2615 11.5627 0019854 76.6854 103.8290 12.96889342521967Epoch: 2025-10-27T23:47Z
TLE epoch observation values (Epoch: 2025-10-27T23:47:02.312Z)
Latitude
-0.85204°
Longitude
158.21429°
Altitude
1,280.953 km
Speed
7.214 km/s
True Right ascension
12h 46m 14s
True Declination
0° 50' 50"
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
21:11:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,286.618 km
Perigee altitude
1,256.243 km
Semi-major axis
7,649.567 km
Eccentricity
0.00199
Inclination
90.2615°
RAAN
11.5627°
Arg. of periapsis
76.6854°
True anomaly
104.04978°
Mean anomaly
103.829°
Eccentric anomaly
103.93941°
Mean motion
3.24405 °/min
Orbital period
110.97 mins
BSTAR
0.0025434
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Other satellites on launch #27 in the year 1965 (1965-04-03 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.OPS 4682 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-10-29 04:34:40.919Z | 154.686° SSE | 2025-10-29 04:41:40.919Z | 74.687° E | 39.239° | 2025-10-29 04:48:40.919Z | 6.571° NNE |
| 11 mins | 2025-10-29 06:27:40.919Z | 230.626° WSW | 2025-10-29 06:32:40.919Z | 280.544° WNW | 24.536° | 2025-10-29 06:38:40.919Z | 334.454° NNW |
| 12 mins | 2025-10-29 16:12:40.919Z | 21.982° NNE | 2025-10-29 16:18:40.919Z | 86.226° E | 31.901° | 2025-10-29 16:24:40.919Z | 147.945° SSE |
| 12 mins | 2025-10-29 18:03:40.919Z | 342.871° N | 2025-10-29 18:09:40.919Z | 275.408° WNW | 32.239° | 2025-10-29 18:15:40.919Z | 218.895° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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