OV1-13 R/B, 3212
Orbit data source: Space-Track
OV1-13 R/B, 3212 is space debris originally from a launch on Sat, 06 Apr 1968 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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3212 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
125 kg wet, 125 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OV1-13 R/B
1 3212U 68026D 25311.76604843 .00000117 00000-0 24050-3 0 9993
2 3212 99.9765 340.4163 3790043 36.5419 344.2393 7.28563446304224Epoch: 2025-11-07T18:23Z
TLE epoch observation values (Epoch: 2025-11-07T18:23:06.584Z)
Latitude
0.00005°
Longitude
17.43355°
Altitude
999.214 km
Speed
8.522 km/s
True Right ascension
22h 41m 39s
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
01:10:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,118.444 km
Perigee altitude
600.311 km
Semi-major axis
11,237.515 km
Eccentricity
0.379
Inclination
99.9765°
RAAN
340.4163°
Arg. of periapsis
36.5419°
True anomaly
323.5697°
Mean anomaly
344.2393°
Eccentric anomaly
335.09446°
Mean motion
1.82196 °/min
Orbital period
197.59 mins
BSTAR
0.0002405
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Other satellites on launch #26 in the year 1968 (1968-04-06 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.OV1-13 R/B 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. |
|---|---|---|---|---|---|---|---|
| 33 mins | 2025-11-08 11:28:38.666Z | 59.806° ENE | 2025-11-08 11:41:38.666Z | 96.593° ESE | 16.062° | 2025-11-08 12:01:38.666Z | 130.493° SE |
| 52 mins | 2025-11-08 14:38:38.666Z | 18.334° NNE | 2025-11-08 14:50:38.666Z | 105.16° ESE | 44.805° | 2025-11-08 15:30:38.666Z | 200.708° SSW |
| 23 mins | 2025-11-08 17:55:38.666Z | 339.433° N | 2025-11-08 18:02:38.666Z | 304.211° NW | 21.427° | 2025-11-08 18:18:38.666Z | 264.86° W |
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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