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

Medium (>0.1 m² and <1 m²)

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

TLE from 1 day ago

0 NIMBUS 2 DEB
1 28206U 66040U   26258.68352036  .00001101  00000-0  18202-2 0  9998
2 28206 100.3707 154.2645 0041983 159.0356 230.1801 13.49171261104206

Epoch: 2026-09-15T16:24Z

TLE epoch observation values (Epoch: 2026-09-15T16:24:16.159Z)

Latitude

28.37718°

Longitude

-92.09297°

Altitude

1,098.792 km

Speed

7.296 km/s

True Right ascension

09h 54m 28s

True Declination

28° 14' 25"

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

09:09:11

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,103.928 km

Perigee altitude

1,041.367 km

Semi-major axis

7,450.784 km

Eccentricity

0.0042

Inclination

100.3707°

RAAN

154.2645°

Arg. of periapsis

159.0356°

True anomaly

229.81183°

Mean anomaly

230.1801°

Eccentric anomaly

229.99584°

Mean motion

3.37474 °/min

Orbital period

106.67 mins

BSTAR

0.0018202

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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	2026-09-16 17:16:07.532Z	173.957° S	2026-09-16 17:22:07.532Z	235.826° WSW	66.023°	2026-09-16 17:28:07.532Z	337.337° NNW
4 mins	2026-09-17 04:32:07.532Z	76.101° E	2026-09-17 04:33:07.532Z	86.297° E	14.503°	2026-09-17 04:36:07.532Z	116.254° SE
11 mins	2026-09-17 06:14:07.532Z	13.624° NNE	2026-09-17 06:19:07.532Z	331.273° NNW	80.801°	2026-09-17 06:25:07.532Z	200.875° SSW
4 mins	2026-09-17 08:02:07.532Z	320.039° NNW	2026-09-17 08:03:07.532Z	309.896° NW	14.516°	2026-09-17 08:06:07.532Z	280.214° WNW

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-09-15T16:24:16.159Z)

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: 1 day ago