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, 0.075 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 NIMBUS 2 DEB
1 28206U 66040U   26305.69632962  .00001185  00000-0  19452-2 0  9991
2 28206 100.3710 203.1037 0050657  42.8047 344.2912 13.49291338110545

Epoch: 2026-11-01T16:42Z

TLE epoch observation values (Epoch: 2026-11-01T16:42:42.879Z)

Latitude

26.49955°

Longitude

-93.76704°

Altitude

1,041.619 km

Speed

7.351 km/s

True Right ascension

13h 11m 34s

True Declination

26° 22' 04"

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

23:52:06

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,109.946 km

Perigee altitude

1,034.464 km

Semi-major axis

7,450.342 km

Eccentricity

0.00507

Inclination

100.371°

RAAN

203.1037°

Arg. of periapsis

42.8047°

True anomaly

344.13307°

Mean anomaly

344.2912°

Eccentric anomaly

344.21223°

Mean motion

3.37504 °/min

Orbital period

106.67 mins

BSTAR

0.0019452

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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.
12 mins	2026-11-02 05:37:46.263Z	28.82° NE	2026-11-02 05:43:46.263Z	99.254° ESE	45.871°	2026-11-02 05:49:46.263Z	171.417° S
9 mins	2026-11-02 07:24:46.263Z	346.342° N	2026-11-02 07:28:46.263Z	295.699° NW	31.458°	2026-11-02 07:33:46.263Z	240.819° WSW
8 mins	2026-11-02 15:52:46.263Z	103.786° ESE	2026-11-02 15:56:46.263Z	56.945° ENE	24.628°	2026-11-02 16:00:46.263Z	13.599° NNE
10 mins	2026-11-02 17:36:46.263Z	184.998° SSW	2026-11-02 17:40:46.263Z	241.172° WSW	55.763°	2026-11-02 17:46:46.263Z	334.195° 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, 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: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-11-01T16:42:42.879Z)

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: 11 hours ago