NIMBUS 2 DEB, 28609

Orbit data source: Space-Track

NIMBUS 2 DEB, 28609 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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https://www.satcat.com/sats-embedded/28609?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28609, 1966-040Y

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: 1 week ago

TLE from 1 week ago

0 NIMBUS 2 DEB
1 28609U 66040Y   26164.00890488  .00000906  00000-0  14800-2 0  9997
2 28609 100.3409  79.4888 0052002 339.0084  37.2660 13.50307112634622

Epoch: 2026-06-13T00:12Z

TLE epoch observation values (Epoch: 2026-06-13T00:12:49.381Z)

Latitude

16.34399°

Longitude

171.9014°

Altitude

1,042.489 km

Speed

7.347 km/s

True Right ascension

05h 05m 44s

True Declination

16° 15' 18"

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

05:23:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,107.187 km

Perigee altitude

1,029.74 km

Semi-major axis

7,446.601 km

Eccentricity

0.0052

Inclination

100.3409°

RAAN

79.4888°

Arg. of periapsis

339.0084°

True anomaly

37.6287°

Mean anomaly

37.266°

Eccentric anomaly

37.44716°

Mean motion

3.37758 °/min

Orbital period

106.59 mins

BSTAR

0.00148

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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.
11 mins	2026-06-22 18:57:39.611Z	192.266° SSW	2026-06-22 19:02:39.611Z	250.464° W	34.23°	2026-06-22 19:08:39.611Z	328.755° NNW
8 mins	2026-06-23 06:10:39.611Z	55.804° ENE	2026-06-23 06:13:39.611Z	89.96° E	22.777°	2026-06-23 06:18:39.611Z	143.575° SSE
11 mins	2026-06-23 07:54:39.611Z	2.381° NNE	2026-06-23 07:59:39.611Z	280.137° WNW	39.805°	2026-06-23 08:05:39.611Z	215.599° SW
4 mins	2026-06-23 16:25:39.611Z	65.229° ENE	2026-06-23 16:26:39.611Z	55.34° ENE	13.518°	2026-06-23 16:29:39.611Z	27.208° NE
11 mins	2026-06-23 18:05:39.611Z	155.603° SSE	2026-06-23 18:10:39.611Z	87.758° E	44.3°	2026-06-23 18:16:39.611Z	347.741° 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, 28609 on other resources

View NIMBUS 2 DEB, 28609 on Heavens-Above

View NIMBUS 2 DEB, 28609 on Keep Track

View NIMBUS 2 DEB, 28609 on Celestrak

View NIMBUS 2 DEB, 28609 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, 28609

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 week ago

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-06-13T00:12:49.381Z)

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, 28609 on other resources

Documentation

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