NIMBUS 2 DEB, 28610

Orbit data source: Space-Track

NIMBUS 2 DEB, 28610 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/28610?theme=dark&initialShowStats=false

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Identifier

28610, 1966-040Z

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: 3 days ago

TLE from 3 days ago

0 NIMBUS 2 DEB
1 28610U 66040Z   26213.54780037  .00001362  00000-0  17953-2 0  9990
2 28610 100.5028 310.4680 0079628  24.5318 349.5777 13.61986328632956

Epoch: 2026-08-01T13:08Z

TLE epoch observation values (Epoch: 2026-08-01T13:08:49.951Z)

Latitude

13.67423°

Longitude

160.53012°

Altitude

972.52 km

Speed

7.395 km/s

True Right ascension

20h 31m 35s

True Declination

13° 35' 52"

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

16:52:09

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,084.766 km

Perigee altitude

966.854 km

Semi-major axis

7,403.947 km

Eccentricity

0.00796

Inclination

100.5028°

RAAN

310.468°

Arg. of periapsis

24.5318°

True anomaly

349.411°

Mean anomaly

349.5777°

Eccentric anomaly

349.49451°

Mean motion

3.40681 °/min

Orbital period

105.67 mins

BSTAR

0.0017953

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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.
6 mins	2026-08-04 04:43:50.399Z	89.003° E	2026-08-04 04:46:50.399Z	58.361° ENE	15.122°	2026-08-04 04:49:50.399Z	26.652° NE
10 mins	2026-08-04 06:25:50.399Z	165.253° S	2026-08-04 06:30:50.399Z	322.493° NNW	44.296°	2026-08-04 06:35:50.399Z	342.924° N
11 mins	2026-08-04 19:14:50.399Z	23.783° NE	2026-08-04 19:19:50.399Z	94.338° ESE	42.513°	2026-08-04 19:25:50.399Z	185.269° SSW
7 mins	2026-08-04 21:00:50.399Z	332.985° NNW	2026-08-04 21:03:50.399Z	297.387° NW	20.614°	2026-08-04 21:07:50.399Z	256.534° W

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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, 28610 on other resources

View NIMBUS 2 DEB, 28610 on Heavens-Above

View NIMBUS 2 DEB, 28610 on Keep Track

View NIMBUS 2 DEB, 28610 on Celestrak

View NIMBUS 2 DEB, 28610 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, 28610

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-08-01T13:08:49.951Z)

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, 28610 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago