OV1-14 R/B, 3177
Orbit data source: Space-Track
OV1-14 R/B, 3177 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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3177 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
Cyl, 1.0 m
Radar Cross Section
1.363 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OV1-14 R/B
1 03177U 68026C 25260.05660595 .00000284 00000-0 40994-3 0 9994
2 03177 99.9802 287.1978 4014637 123.2865 305.3107 6.98005360458149Epoch: 2025-09-17T01:21Z
TLE epoch observation values (Epoch: 2025-09-17T01:21:30.754Z)
Latitude
21.62978°
Longitude
-93.40473°
Altitude
4,153.768 km
Speed
6.424 km/s
True Right ascension
18h 52m 50s
True Declination
21° 33' 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
04:11:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,827.276 km
Perigee altitude
542.862 km
Semi-major axis
11,563.206 km
Eccentricity
0.40146
Inclination
99.9802°
RAAN
287.1978°
Arg. of periapsis
123.2865°
True anomaly
258.69887°
Mean anomaly
305.3107°
Eccentric anomaly
282.888°
Mean motion
1.74552 °/min
Orbital period
206.24 mins
BSTAR
0.00040994
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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.OV1-14 R/B 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-17 15:38:44.635Z | 345.57° N | 2025-09-17 15:41:44.635Z | 274.959° WNW | 24.733° | 2025-09-17 15:44:44.635Z | 230.383° WSW |
| 35 mins | 2025-09-18 01:07:44.635Z | 154.081° SSE | 2025-09-18 01:34:44.635Z | 69.585° E | 44.717° | 2025-09-18 01:42:44.635Z | 348.233° N |
| 17 mins | 2025-09-18 04:43:44.635Z | 234.895° WSW | 2025-09-18 04:53:44.635Z | 259.529° W | 13.528° | 2025-09-18 05:00:44.635Z | 285.988° WNW |
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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