NIMBUS 2 DEB, 28612

Orbit data source: Space-Track

NIMBUS 2 DEB, 28612 is space debris in SSO originally from a launch on Sun, 15 May 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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Iframe URL

https://www.satcat.com/sats-embedded/28612?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28612, 1966-040AB

Orbit

SSO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-05-15 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 28612U 66040AB  26065.60676568  .00003582  00000-0  36364-2 0  9990
2 28612 100.3864 301.3430 0043124 304.4953  84.2581 13.77290516686198

Epoch: 2026-03-06T14:33Z

TLE epoch observation values (Epoch: 2026-03-06T14:33:44.554Z)

Latitude

28.76757°

Longitude

-87.17824°

Altitude

973.928 km

Speed

7.369 km/s

True Right ascension

19h 42m 23s

True Declination

28° 37' 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

19:48:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,002.506 km

Perigee altitude

939.123 km

Semi-major axis

7,348.952 km

Eccentricity

0.00431

Inclination

100.3864°

RAAN

301.343°

Arg. of periapsis

304.4953°

True anomaly

84.75004°

Mean anomaly

84.2581°

Eccentric anomaly

84.50405°

Mean motion

3.44513 °/min

Orbital period

104.5 mins

BSTAR

0.0036364

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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

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NIMBUS 2 DEB Visibility forecast

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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.
8 mins	2026-03-07 16:41:23.336Z	217.527° SW	2026-03-07 16:45:23.336Z	264.362° W	22.14°	2026-03-07 16:49:23.336Z	311.28° NW
9 mins	2026-03-08 03:39:23.336Z	46.212° ENE	2026-03-08 03:43:23.336Z	97.87° ESE	26.552°	2026-03-08 03:48:23.336Z	155.187° SSE
9 mins	2026-03-08 05:22:23.336Z	354.598° N	2026-03-08 05:26:23.336Z	294.595° NW	34.489°	2026-03-08 05:31:23.336Z	227.583° WSW
10 mins	2026-03-08 15:21:23.336Z	156.492° SSE	2026-03-08 15:26:23.336Z	45.984° ENE	44.342°	2026-03-08 15:31:23.336Z	347.534° N

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out NIMBUS 2 DEB, 28612 on other resources

View NIMBUS 2 DEB, 28612 on Heavens-Above

View NIMBUS 2 DEB, 28612 on Keep Track

View NIMBUS 2 DEB, 28612 on Celestrak

View NIMBUS 2 DEB, 28612 on Gunter's Space Page

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

NIMBUS 2 DEB, 28612

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-03-06T14:33:44.554Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

NIMBUS 2 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out NIMBUS 2 DEB, 28612 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago