NIMBUS 2 DEB, 27406

Orbit data source: Space-Track

NIMBUS 2 DEB, 27406 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/27406?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

27406, 1966-040AL

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: 2 days ago

TLE from 2 days ago

0 NIMBUS 2 DEB
1 27406U 66040AL  25363.85103671  .00003746  00000-0  44157-2 0  9998
2 27406 100.2972  30.7066 0042704 275.1552 267.5129 13.68286017302186

Epoch: 2025-12-29T20:25Z

TLE epoch observation values (Epoch: 2025-12-29T20:25:29.571Z)

Latitude

-2.26996°

Longitude

165.38016°

Altitude

1,010.346 km

Speed

7.346 km/s

True Right ascension

14h 01m 11s

True Declination

-2° 15' 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

01:04:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,034.56 km

Perigee altitude

971.519 km

Semi-major axis

7,381.177 km

Eccentricity

0.00427

Inclination

100.2972°

RAAN

30.7066°

Arg. of periapsis

275.1552°

True anomaly

267.02413°

Mean anomaly

267.5129°

Eccentric anomaly

267.2685°

Mean motion

3.42259 °/min

Orbital period

105.18 mins

BSTAR

0.0044157

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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	2026-01-01 02:01:58.595Z	171.227° S	2026-01-01 02:07:58.595Z	270.807° WNW	43.636°	2026-01-01 02:13:58.595Z	340.413° N
11 mins	2026-01-01 14:48:58.595Z	20.022° NNE	2026-01-01 14:53:58.595Z	79.407° E	43.921°	2026-01-01 14:59:58.595Z	190.135° SSW
6 mins	2026-01-01 16:34:58.595Z	327.858° NNW	2026-01-01 16:36:58.595Z	305.349° NW	18.038°	2026-01-01 16:40:58.595Z	263.488° W
9 mins	2026-01-02 00:53:58.595Z	117.154° SE	2026-01-02 00:57:58.595Z	63.832° ENE	29.241°	2026-01-02 01:02:58.595Z	4.997° NNE

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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, 27406 on other resources

View NIMBUS 2 DEB, 27406 on Heavens-Above

View NIMBUS 2 DEB, 27406 on Keep Track

View NIMBUS 2 DEB, 27406 on Celestrak

View NIMBUS 2 DEB, 27406 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, 27406

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-12-29T20:25:29.571Z)

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, 27406 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago