NIMBUS 2 DEB, 28620

Orbit data source: Space-Track

NIMBUS 2 DEB, 28620 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/28620?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28620, 1966-040AK

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 28620U 66040AK  26261.53906394  .00001498  00000-0  23163-2 0  9999
2 28620 100.4321 178.1156 0038739 153.9179  22.2999 13.52751204 63838

Epoch: 2026-09-18T12:56Z

TLE epoch observation values (Epoch: 2026-09-18T12:56:15.124Z)

Latitude

3.46223°

Longitude

167.22702°

Altitude

1,037.878 km

Speed

7.346 km/s

True Right ascension

23h 55m 00s

True Declination

3° 26' 32"

Sunlit

Object was in full shadow 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

17:06:09

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,088.303 km

Perigee altitude

1,030.677 km

Semi-major axis

7,437.627 km

Eccentricity

0.00387

Inclination

100.4321°

RAAN

178.1156°

Arg. of periapsis

153.9179°

True anomaly

22.4691°

Mean anomaly

22.2999°

Eccentric anomaly

22.38443°

Mean motion

3.3837 °/min

Orbital period

106.39 mins

BSTAR

0.0023163

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

THOR AGENA B R/B, 2174

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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.
12 mins	2026-09-20 07:15:59.656Z	21.969° NNE	2026-09-20 07:21:59.656Z	122.095° SE	66.904°	2026-09-20 07:27:59.656Z	186.884° SSW
7 mins	2026-09-20 09:02:59.656Z	334.916° NNW	2026-09-20 09:05:59.656Z	300.673° NW	21.063°	2026-09-20 09:09:59.656Z	258.812° W
10 mins	2026-09-20 17:27:59.656Z	120.918° SE	2026-09-20 17:32:59.656Z	54.654° ENE	35.504°	2026-09-20 17:37:59.656Z	2.37° NNE
10 mins	2026-09-20 19:12:59.656Z	202.314° SSW	2026-09-20 19:16:59.656Z	256° W	39.206°	2026-09-20 19:22:59.656Z	327.585° NNW

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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, 28620 on other resources

View NIMBUS 2 DEB, 28620 on Heavens-Above

View NIMBUS 2 DEB, 28620 on Keep Track

View NIMBUS 2 DEB, 28620 on Celestrak

View NIMBUS 2 DEB, 28620 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, 28620

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: 2026-09-18T12:56:15.124Z)

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, 28620 on other resources

Documentation

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