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   25336.12680691  .00001778  00000-0  29307-2 0  9992
2 28206 100.3716 215.6826 0042834 137.0858  19.1724 13.48325125 65437

Epoch: 2025-12-02T03:02Z

TLE epoch observation values (Epoch: 2025-12-02T03:02:36.117Z)

Latitude

23.19265°

Longitude

-76.71005°

Altitude

1,050.939 km

Speed

7.343 km/s

True Right ascension

02h 40m 37s

True Declination

23° 04' 24"

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

15:00:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,107.694 km

Perigee altitude

1,043.838 km

Semi-major axis

7,453.903 km

Eccentricity

0.00428

Inclination

100.3716°

RAAN

215.6826°

Arg. of periapsis

137.0858°

True anomaly

19.33442°

Mean anomaly

19.1724°

Eccentric anomaly

19.25333°

Mean motion

3.37262 °/min

Orbital period

106.74 mins

BSTAR

0.0029307

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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	2025-12-03 03:49:36.290Z	45.763° ENE	2025-12-03 03:54:36.290Z	98.26° ESE	20.68°	2025-12-03 03:58:36.290Z	140.082° SSE
10 mins	2025-12-03 05:35:36.290Z	2.323° NNE	2025-12-03 05:39:36.290Z	301.202° NW	40.316°	2025-12-03 05:45:36.290Z	214.797° SW
4 mins	2025-12-03 14:06:36.290Z	70.924° E	2025-12-03 14:08:36.290Z	51.619° ENE	13.132°	2025-12-03 14:10:36.290Z	32.658° NE
11 mins	2025-12-03 15:47:36.290Z	154.162° SSE	2025-12-03 15:52:36.290Z	65.014° ENE	44.142°	2025-12-03 15:58:36.290Z	348.037° 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: 2025-12-02T03:02:36.117Z)

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