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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Identifier
3177, 1968-026C
Orbit
Active
Country
Flag of USUS
Related business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
125 kg wet, 125 kg dry
Launch date (UTC)
1968-04-06 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.0 m
Radar Cross Section
1.363 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 OV1-14 R/B
1 03177U 68026C   25258.05019535  .00000235  00000-0  33846-3 0  9997
2 03177  99.9807 286.5845 4014855 124.7894 303.5686  6.98004147458009
Epoch: 2025-09-15T01:12Z
TLE epoch observation values (Epoch: 2025-09-15T01:12:16.878Z)
Latitude
21.23759°
Longitude
-89.65348°
Altitude
4,304.465 km
Speed
6.34 km/s
True Right ascension
18h 50m 42s
True Declination
21° 09' 37"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
08:27:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,827.547 km
Perigee altitude
542.617 km
Semi-major axis
11,563.219 km
Eccentricity
0.40149
Inclination
99.9807°
RAAN
286.5845°
Arg. of periapsis
124.7894°
True anomaly
256.79845°
Mean anomaly
303.5686°
Eccentric anomaly
280.9868°
Mean motion
1.74552 °/min
Orbital period
206.24 mins
BSTAR
0.00033846
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Other satellites on launch #26 in the year 1968 (1968-04-06 UTC)

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