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 (58 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 OV1-14 R/B
1 03177U 68026C   26134.60513135 -.00000217  00000-0 -29468-3 0  9994
2 03177  99.9669   0.3552 4013648 303.6801  35.6829  6.98162165474866
Epoch: 2026-05-14T14:31Z
TLE epoch observation values (Epoch: 2026-05-14T14:31:23.348Z)
Latitude
19.68286°
Longitude
-93.42844°
Altitude
2,483.956 km
Speed
7.452 km/s
True Right ascension
23h 47m 04s
True Declination
19° 35' 43"
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
17:06:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,823.705 km
Perigee altitude
542.968 km
Semi-major axis
11,561.474 km
Eccentricity
0.40136
Inclination
99.9669°
RAAN
0.3552°
Arg. of periapsis
303.6801°
True anomaly
76.32822°
Mean anomaly
35.6829°
Eccentric anomaly
54.3757°
Mean motion
1.74592 °/min
Orbital period
206.2 mins
BSTAR
-0.00029468
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Other satellites on launch #26 in the year 1968 (1968-04-06 UTC)

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