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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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
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OV1-13 R/B
1 03212U 68026D 26260.06551731 .00000061 00000-0 12764-3 0 9994
2 03212 99.9741 81.9467 3788773 147.4652 243.0017 7.28625532327049Epoch: 2026-09-17T01:34Z
TLE epoch observation values (Epoch: 2026-09-17T01:34:20.695Z)
Latitude
-0.00001°
Longitude
62.35237°
Altitude
7,762.672 km
Speed
4.574 km/s
True Right ascension
05h 27m 47s
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
09:55:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,116.137 km
Perigee altitude
601.342 km
Semi-major axis
11,236.876 km
Eccentricity
0.37888
Inclination
99.9741°
RAAN
81.9467°
Arg. of periapsis
147.4652°
True anomaly
212.61083°
Mean anomaly
243.0017°
Eccentric anomaly
227.09969°
Mean motion
1.82211 °/min
Orbital period
197.57 mins
BSTAR
0.00012764
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-18 01:36:18.269Z | 3.227° NNE | 2026-09-18 01:40:18.269Z | 274.057° WNW | 45.781° | 2026-09-18 01:43:18.269Z | 217.124° SW |
| 46 mins | 2026-09-18 10:29:18.269Z | 136.026° SSE | 2026-09-18 11:03:18.269Z | 64.529° ENE | 61.401° | 2026-09-18 11:15:18.269Z | 354.582° N |
| 53 mins | 2026-09-18 13:36:18.269Z | 194.116° SSW | 2026-09-18 14:13:18.269Z | 257.815° W | 38.888° | 2026-09-18 14:29:18.269Z | 323.556° NNW |
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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