OPS 4682 DEB, 38429
Orbit data source: Space-Track
OPS 4682 DEB, 38429 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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
38429 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Edit Sat Name
Focus sentinelFocus sentinel
Create New Watchlist
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, 0.079 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OPS 4682 DEB
1 38429U 65027EJ 26308.45133786 .00000046 00000-0 12947-3 0 9998
2 38429 90.2379 3.7807 0042555 27.5948 332.7419 12.98029277607615Epoch: 2026-11-04T10:49Z
TLE epoch observation values (Epoch: 2026-11-04T10:49:55.591Z)
Latitude
-0.00002°
Longitude
157.59961°
Altitude
1,243.791 km
Speed
7.247 km/s
True Right ascension
00h 15m 07s
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
22:37:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,299.481 km
Perigee altitude
1,234.414 km
Semi-major axis
7,645.085 km
Eccentricity
0.00426
Inclination
90.2379°
RAAN
3.7807°
Arg. of periapsis
27.5948°
True anomaly
332.5175°
Mean anomaly
332.7419°
Eccentric anomaly
332.62981°
Mean motion
3.24691 °/min
Orbital period
110.87 mins
BSTAR
0.00012947
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #27 in the year 1965 (1965-04-03 UTC)
Did you know?
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
Loading observer location...
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 | 2026-11-07 03:40:08.373Z | 161.839° S | 2026-11-07 03:47:08.373Z | 84.661° E | 64.938° | 2026-11-07 03:54:08.373Z | 4.13° NNE |
| 9 mins | 2026-11-07 05:34:08.373Z | 240.286° WSW | 2026-11-07 05:38:08.373Z | 278.088° WNW | 22.289° | 2026-11-07 05:43:08.373Z | 324.93° NNW |
| 13 mins | 2026-11-07 15:18:08.373Z | 19.653° NNE | 2026-11-07 15:24:08.373Z | 91.22° ESE | 45.933° | 2026-11-07 15:31:08.373Z | 157.98° S |
| 11 mins | 2026-11-07 17:09:08.373Z | 338° N | 2026-11-07 17:14:08.373Z | 286.797° WNW | 33.791° | 2026-11-07 17:20:08.373Z | 227.237° WSW |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|