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: 12 hours ago

TLE from 12 hours ago

0 NIMBUS 2 DEB
1 27406U 66040AL  26215.61708545  .00003179  00000-0  36736-2 0  9994
2 27406 100.2937 261.7783 0042789 100.3005  52.7720 13.69632432331847

Epoch: 2026-08-03T14:48Z

TLE epoch observation values (Epoch: 2026-08-03T14:48:36.182Z)

Latitude

26.11116°

Longitude

-87.48962°

Altitude

984.931 km

Speed

7.371 km/s

True Right ascension

05h 47m 26s

True Declination

25° 58' 47"

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

16:53:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,029.76 km

Perigee altitude

966.635 km

Semi-major axis

7,376.335 km

Eccentricity

0.00428

Inclination

100.2937°

RAAN

261.7783°

Arg. of periapsis

100.3005°

True anomaly

53.16368°

Mean anomaly

52.772°

Eccentric anomaly

52.96771°

Mean motion

3.42596 °/min

Orbital period

105.08 mins

BSTAR

0.0036736

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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	2026-08-04 04:12:23.279Z	216.373° SW	2026-08-04 04:16:23.279Z	260.942° W	21.931°	2026-08-04 04:21:23.279Z	316.469° NNW
8 mins	2026-08-04 15:14:23.279Z	48.471° ENE	2026-08-04 15:17:23.279Z	89.642° E	27.748°	2026-08-04 15:22:23.279Z	155.341° SSE
9 mins	2026-08-04 16:57:23.279Z	352.751° N	2026-08-04 17:01:23.279Z	295.227° NW	32.067°	2026-08-04 17:06:23.279Z	230.667° WSW
4 mins	2026-08-05 01:20:23.279Z	74.921° E	2026-08-05 01:22:23.279Z	53.157° ENE	14.518°	2026-08-05 01:24:23.279Z	32.108° NE

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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: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-08-03T14:48:36.182Z)

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: 12 hours ago