NIMBUS 2 DEB, 28208

Orbit data source: Space-Track

NIMBUS 2 DEB, 28208 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/28208?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28208, 1966-040W

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 (59 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: 8 hours ago

TLE from 8 hours ago

0 NIMBUS 2 DEB
1 28208U 66040W   25286.98088985  .00002771  00000-0  34599-2 0  9993
2 28208 100.3271 302.7686 0047054 135.6581 255.6733 13.64986586221470

Epoch: 2025-10-13T23:32Z

TLE epoch observation values (Epoch: 2025-10-13T23:32:28.883Z)

Latitude

30.31027°

Longitude

-79.21093°

Altitude

1,030.082 km

Speed

7.335 km/s

True Right ascension

19h 46m 44s

True Declination

30° 09' 58"

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

01:38:09

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,049.727 km

Perigee altitude

980.152 km

Semi-major axis

7,393.077 km

Eccentricity

0.00471

Inclination

100.3271°

RAAN

302.7686°

Arg. of periapsis

135.6581°

True anomaly

255.15164°

Mean anomaly

255.6733°

Eccentric anomaly

255.41239°

Mean motion

3.41433 °/min

Orbital period

105.44 mins

BSTAR

0.0034599

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

THOR AGENA B R/B, 2174

NIMBUS 2 DEB, 31579

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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	2025-10-14 14:03:17.005Z	18.398° NNE	2025-10-14 14:08:17.005Z	63.586° ENE	44.258°	2025-10-14 14:14:17.005Z	192.602° SSW
6 mins	2025-10-14 15:49:17.005Z	330.73° NNW	2025-10-14 15:52:17.005Z	297.451° NW	16.08°	2025-10-14 15:55:17.005Z	267.05° W
9 mins	2025-10-15 00:10:17.005Z	119.632° SE	2025-10-15 00:14:17.005Z	61.163° ENE	31.049°	2025-10-15 00:19:17.005Z	2.598° NNE
10 mins	2025-10-15 01:53:17.005Z	201.568° SSW	2025-10-15 01:58:17.005Z	267.633° W	30.116°	2025-10-15 02:03:17.005Z	324.895° NNW

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, 28208 on other resources

View NIMBUS 2 DEB, 28208 on Heavens-Above

View NIMBUS 2 DEB, 28208 on Keep Track

View NIMBUS 2 DEB, 28208 on Celestrak

View NIMBUS 2 DEB, 28208 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, 28208

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2025-10-13T23:32:28.883Z)

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, 28208 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago