DELTA 1 DEB, 2154

Orbit data source: Space-Track

DELTA 1 DEB, 2154 is space debris in SSO originally from a launch on Thu, 03 Feb 1966 UTC launched from the Air Force Eastern Test Range (AFETR). 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/2154?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2154, 1966-008E

Orbit

SSO

Last TLE update

12 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-02-03 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 12 hours ago

0 DELTA 1 DEB
1 02154U 66008E   25221.55934635  .00001329  00000-0  22256-3 0  9999
2 02154  97.8438 343.5208 0046197 225.0701 134.6755 14.70696902133194

Epoch: 2025-08-09T13:25Z

TLE epoch observation values (Epoch: 2025-08-09T13:25:27.524Z)

Latitude

0.00001°

Longitude

-176.13719°

Altitude

684.792 km

Speed

7.502 km/s

True Right ascension

22h 54m 04s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

54.67642°

Longitude

15.49233°

Altitude

672.721 km

Speed

7.523 km/s

Apparent Right ascension

07h 04m 34s

Apparent Declination

20° 04' 40"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:40:04

Azimuth

311.262° NW

Elevation

-13.404°

Doppler factor

Orbital elements

Apogee altitude

688.39 km

Perigee altitude

623.4 km

Semi-major axis

7,034.032 km

Eccentricity

0.00462

Inclination

97.8438°

RAAN

343.5208°

Arg. of periapsis

225.0701°

True anomaly

135.05042°

Mean anomaly

134.6755°

Eccentric anomaly

134.86311°

Mean motion

3.67906 °/min

Orbital period

97.85 mins

BSTAR

0.00022256

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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

ESSA 1 (OT-3), 1982

DELTA 1 R/B, 1983

DELTA 1 DEB, 2085 (Decayed)

DELTA 1 DEB, 2118

DELTA 1 DEB Visibility forecast

Observer location: undefined°, undefined°

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.
7 mins	2025-08-10 07:31:23.949Z	129.529° SE	2025-08-10 07:34:23.949Z	81.426° E	29.13°	2025-08-10 07:38:23.949Z	9.763° NNE
6 mins	2025-08-10 09:09:23.949Z	227.053° WSW	2025-08-10 09:11:23.949Z	259.57° W	21.243°	2025-08-10 09:15:23.949Z	318.144° NNW
7 mins	2025-08-10 21:02:23.949Z	14.895° NNE	2025-08-10 21:05:23.949Z	164.238° S	44.512°	2025-08-10 21:09:23.949Z	191.678° SSW

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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Check out DELTA 1 DEB, 2154 on other resources

View DELTA 1 DEB, 2154 on Heavens-Above

View DELTA 1 DEB, 2154 on Keep Track

View DELTA 1 DEB, 2154 on Celestrak

View DELTA 1 DEB, 2154 on Gunter's Space Page

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