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)

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Last TLE update: 2 days ago

TLE from 2 days ago

0 NIMBUS 2 DEB
1 27406U 66040AL  26144.60101689  .00003087  00000-0  36066-2 0  9994
2 27406 100.2844 186.0058 0032901 267.3986 244.8911 13.69158175322129

Epoch: 2026-05-24T14:25Z

TLE epoch observation values (Epoch: 2026-05-24T14:25:27.859Z)

Latitude

27.60292°

Longitude

-87.14543°

Altitude

1,016.238 km

Speed

7.341 km/s

True Right ascension

00h 45m 41s

True Declination

27° 28' 01"

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

16:14:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,024.176 km

Perigee altitude

975.627 km

Semi-major axis

7,378.039 km

Eccentricity

0.00329

Inclination

100.2844°

RAAN

186.0058°

Arg. of periapsis

267.3986°

True anomaly

244.55031°

Mean anomaly

244.8911°

Eccentric anomaly

244.72064°

Mean motion

3.42477 °/min

Orbital period

105.12 mins

BSTAR

0.0036066

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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	2026-05-26 15:22:48.197Z	23.916° NE	2026-05-26 15:28:48.197Z	118.96° SE	40.895°	2026-05-26 15:33:48.197Z	181.141° SSW
7 mins	2026-05-26 17:08:48.197Z	333.805° NNW	2026-05-26 17:11:48.197Z	296.718° NW	21.315°	2026-05-26 17:15:48.197Z	253.992° W
8 mins	2026-05-27 01:28:48.197Z	103.371° ESE	2026-05-27 01:31:48.197Z	64.813° ENE	24.826°	2026-05-27 01:36:48.197Z	8.688° NNE
10 mins	2026-05-27 03:10:48.197Z	189.954° SSW	2026-05-27 03:14:48.197Z	244.438° WSW	37.087°	2026-05-27 03:20:48.197Z	331.889° 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, 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: 2026-05-24T14:25:27.859Z)

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