NIMBUS 2 DEB, 28206

Orbit data source: Space-Track

NIMBUS 2 DEB, 28206 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/28206?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28206, 1966-040U

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: 14 hours ago

TLE from 14 hours ago

0 NIMBUS 2 DEB
1 28206U 66040U   26079.14938223  .00001247  00000-0  20653-2 0  9992
2 28206 100.3750 327.7974 0045323 241.1160 274.8164 13.48719251 79994

Epoch: 2026-03-20T03:35Z

TLE epoch observation values (Epoch: 2026-03-20T03:35:06.624Z)

Latitude

24.18292°

Longitude

-78.97716°

Altitude

1,077.075 km

Speed

7.317 km/s

True Right ascension

10h 09m 57s

True Declination

24° 03' 37"

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

22:29:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,108.09 km

Perigee altitude

1,040.536 km

Semi-major axis

7,452.45 km

Eccentricity

0.00453

Inclination

100.375°

RAAN

327.7974°

Arg. of periapsis

241.116°

True anomaly

274.29863°

Mean anomaly

274.8164°

Eccentric anomaly

274.55754°

Mean motion

3.37361 °/min

Orbital period

106.71 mins

BSTAR

0.0020653

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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.
9 mins	2026-03-21 04:22:03.730Z	45.004° ENE	2026-03-21 04:27:03.730Z	102.732° ESE	24.493°	2026-03-21 04:31:03.730Z	146.249° SSE
11 mins	2026-03-21 06:07:03.730Z	0.801° NNE	2026-03-21 06:12:03.730Z	289.34° WNW	37.64°	2026-03-21 06:18:03.730Z	219.927° SW
5 mins	2026-03-21 14:38:03.730Z	74.252° E	2026-03-21 14:40:03.730Z	53.849° ENE	15.884°	2026-03-21 14:43:03.730Z	25.095° NE
11 mins	2026-03-21 16:19:03.730Z	161.108° S	2026-03-21 16:24:03.730Z	113.139° SE	44.957°	2026-03-21 16:30:03.730Z	345.027° 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, 28206 on other resources

View NIMBUS 2 DEB, 28206 on Heavens-Above

View NIMBUS 2 DEB, 28206 on Keep Track

View NIMBUS 2 DEB, 28206 on Celestrak

View NIMBUS 2 DEB, 28206 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, 28206

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-03-20T03:35:06.624Z)

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, 28206 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago