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: 23 hours ago

TLE from 23 hours ago
0 OV1-14 R/B
1 03177U 68026C   26081.60264089 -.00000126  00000-0 -15979-3 0  9997
2 03177  99.9879 344.1563 4020011 343.4175  22.3338  6.98134543471165
Epoch: 2026-03-22T14:27Z
TLE epoch observation values (Epoch: 2026-03-22T14:27:48.172Z)
Latitude
35.49678°
Longitude
-60.07942°
Altitude
1,419.973 km
Speed
8.238 km/s
True Right ascension
22h 27m 54s
True Declination
35° 20' 53"
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
18:22:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,831.488 km
Perigee altitude
535.793 km
Semi-major axis
11,561.778 km
Eccentricity
0.402
Inclination
99.9879°
RAAN
344.1563°
Arg. of periapsis
343.4175°
True anomaly
52.6442°
Mean anomaly
22.3338°
Eccentric anomaly
35.81055°
Mean motion
1.74585 °/min
Orbital period
206.2 mins
BSTAR
-0.00015979
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Other satellites on launch #26 in the year 1968 (1968-04-06 UTC)

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