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)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago

0 NIMBUS 2 DEB
1 28612U 66040AB  26052.60319931  .00002716  00000-0  27734-2 0  9993
2 28612 100.3859 287.1505 0044298 334.4719  54.4998 13.77204058684401

Epoch: 2026-02-21T14:28Z

TLE epoch observation values (Epoch: 2026-02-21T14:28:36.420Z)

Latitude

28.90633°

Longitude

-87.3027°

Altitude

958.474 km

Speed

7.385 km/s

True Right ascension

18h 45m 29s

True Declination

28° 45' 54"

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

13:57:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,003.678 km

Perigee altitude

938.567 km

Semi-major axis

7,349.259 km

Eccentricity

0.00443

Inclination

100.3859°

RAAN

287.1505°

Arg. of periapsis

334.4719°

True anomaly

54.91439°

Mean anomaly

54.4998°

Eccentric anomaly

54.70696°

Mean motion

3.44491 °/min

Orbital period

104.5 mins

BSTAR

0.0027734

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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.
11 mins	2026-02-22 14:51:32.997Z	141.596° SSE	2026-02-22 14:56:32.997Z	84.75° E	37.564°	2026-02-22 15:02:32.997Z	355.267° N
7 mins	2026-02-22 16:37:32.997Z	228.693° WSW	2026-02-22 16:40:32.997Z	268.195° W	21.648°	2026-02-22 16:44:32.997Z	313.206° NW
9 mins	2026-02-23 03:34:32.997Z	48.427° ENE	2026-02-23 03:38:32.997Z	103.045° ESE	26.635°	2026-02-23 03:43:32.997Z	156.964° SSE
10 mins	2026-02-23 05:16:32.997Z	358.164° N	2026-02-23 05:21:32.997Z	287.134° WNW	34.272°	2026-02-23 05:26:32.997Z	226.621° WSW

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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: 20 hours ago

TLE from 20 hours ago

TLE epoch observation values (Epoch: 2026-02-21T14:28:36.420Z)

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: 20 hours ago