OV1-9 R/B, 2622

Orbit data source: Space-Track

OV1-9 R/B, 2622 is space debris in LEO originally from a launch on Sun, 11 Dec 1966 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
2622, 1966-111D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
125 kg wet, 125 kg dry
Launch date (UTC)
1966-12-11 (59 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: 13 hours ago

TLE from 13 hours ago
0 OV1-9 R/B
1 02622U 66111D   26050.35772604  .00000572  00000-0  23710-3 0  9994
2 02622  99.0957  23.1702 2221331 243.6265  92.0432 10.49774745232533
Epoch: 2026-02-19T08:35Z
TLE epoch observation values (Epoch: 2026-02-19T08:35:07.529Z)
Latitude
0.00001°
Longitude
105.07866°
Altitude
2,920.703 km
Speed
6.365 km/s
True Right ascension
01h 32m 40s
True Declination
0° 00' 00"
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
00:57:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,386.522 km
Perigee altitude
473.385 km
Semi-major axis
8,808.09 km
Eccentricity
0.22213
Inclination
99.0957°
RAAN
23.1702°
Arg. of periapsis
243.6265°
True anomaly
116.47284°
Mean anomaly
92.0432°
Eccentric anomaly
104.37217°
Mean motion
2.62555 °/min
Orbital period
137.11 mins
BSTAR
0.0002371
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Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)

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