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.

Loading next visibility...

OV1-9 R/B details

Identifier	2622, 1966-111D
Orbit	LEO
Last TLE update	13 hours ago
Origin	USAF OAR (US)
Manufacturer	ABL
Mission	Spacecraft
Bus & Motor	ALTAIR, Unknown motor
Mass	125 kg wet, 125 kg dry
Launch date (UTC)	1966-12-11 (58 years ago)
Launch vehicle	Unknown
Launch site	Air Force Western Test Range (AFWTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 2.1 m
Radar Cross Section	1.347 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 13 hours ago

0 OV1-9 R/B
1 02622U 66111D   25015.40108297  .00002184  00000-0  86059-3 0  9997
2 02622  99.0952 158.4680 2226275 145.7981 230.8926 10.48751049190583

Epoch: 2025-01-15T09:37Z

Definitive object data (Epoch: 2025-01-15T09:37:33.568Z)

Latitude	0.00003°
Longitude	-101.01583°
Altitude	3,892.614 km
Speed	5.695 km/s
True Right ascension	10h 33m 52s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-80.84973°
Longitude	-2.57024°
Altitude	3,211.801 km
Speed	6.169 km/s
Apparent Right ascension	12h 22m 26s
Apparent Declination	-69° 04' 11"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	23:13:41
Azimuth	191.983° SSW
Elevation	-59.438°
Doppler factor	1

Orbital elements

Apogee altitude	4,397.886 km
Perigee altitude	473.487 km
Semi-major axis	8,813.823 km
Eccentricity	0.2226275
Inclination	99.0952°
RAAN	158.468°
Arg. of periapsis	145.7981°
True anomaly	214.29406°
Mean anomaly	230.8926°
Eccentric anomaly	222.30679°
Mean motion	2.62299 °/min
BSTAR	0.00086059
Orbital period	137.25 mins

Loading maneuver chart data...

Loading historical data...

Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)

OV1-9, 2610

OV1-10, 2611 (Decayed)

OV1-10 R/B, 2621

OV1-9 R/B, 2622

OV1-9 R/B Visibility forecast

Observer location: undefined°, undefined

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.
10 mins	2025-01-16 06:30:40.070Z	83.762° E	2025-01-16 06:36:40.070Z	56.053° ENE	14.726°	2025-01-16 06:40:40.070Z	31.333° NE
26 mins	2025-01-16 08:33:40.070Z	149.314° SSE	2025-01-16 08:50:40.070Z	71.955° E	43.151°	2025-01-16 08:59:40.070Z	352.833° N
23 mins	2025-01-16 10:50:40.070Z	204.678° SW	2025-01-16 11:04:40.070Z	258.62° W	29.194°	2025-01-16 11:13:40.070Z	317.943° NNW

Authenticating...

Click to sort rows by NORAD ID header in ascending order	Click to sort rows by Common name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in ascending order

Check out OV1-9 R/B, 2622 on other resources

View OV1-9 R/B, 2622 on Heavens-Above

View OV1-9 R/B, 2622 on Keep Track

View OV1-9 R/B, 2622 on Celestrak

View OV1-9 R/B, 2622 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.