DELTA 1 DEB, 2775

Orbit data source: Space-Track

DELTA 1 DEB, 2775 is space debris in SSO originally from a launch on Sun, 02 Oct 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/2775?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

2775, 1966-087D

Orbit

SSO

Last TLE update

2 days ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

1 kg wet, 1 kg dry

Launch date (UTC)

1966-10-02 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Cable, 1.8 m

Radar Cross Section

3.500 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 DELTA 1 DEB
1  2775U 66087D   25197.96553225 -.00000034  00000-0  34940-4 0  9991
2  2775 100.9270 212.9137 0125508  96.2483 329.2300 12.71684602728160

Epoch: 2025-07-16T23:10Z

TLE epoch observation values (Epoch: 2025-07-16T23:10:21.986Z)

Latitude

62.70344°

Longitude

-91.56881°

Altitude

1,302.406 km

Speed

7.25 km/s

True Right ascension

12h 44m 14s

True Declination

62° 34' 23"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-19.63895°

Longitude

-63.85368°

Altitude

1,417.512 km

Speed

7.135 km/s

Apparent Right ascension

17h 07m 21s

Apparent Declination

-59° 37' 35"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:37:04

Azimuth

149.247° SSE

Elevation

-23.931°

Doppler factor

Orbital elements

Apogee altitude

1,469.833 km

Perigee altitude

1,275.279 km

Semi-major axis

7,750.693 km

Eccentricity

0.01255

Inclination

100.927°

RAAN

212.9137°

Arg. of periapsis

96.2483°

True anomaly

328.48419°

Mean anomaly

329.23°

Eccentric anomaly

328.85811°

Mean motion

3.18077 °/min

Orbital period

113.18 mins

BSTAR

0.00003494

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Other satellites on launch #87 in the year 1966 (1966-10-02 UTC)

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.
14 mins	2025-07-19 00:02:24.185Z	135.373° SSE	2025-07-19 00:09:24.185Z	64.535° ENE	36.656°	2025-07-19 00:16:24.185Z	354.909° N
12 mins	2025-07-19 01:55:24.185Z	206.33° SW	2025-07-19 02:00:24.185Z	256.15° W	29.183°	2025-07-19 02:07:24.185Z	324.786° NNW
13 mins	2025-07-19 13:46:24.185Z	23.345° NE	2025-07-19 13:52:24.185Z	129.423° SE	43.294°	2025-07-19 13:59:24.185Z	188.99° SSW
9 mins	2025-07-19 15:38:24.185Z	343.705° N	2025-07-19 15:42:24.185Z	305.547° NW	22.125°	2025-07-19 15:47:24.185Z	259.122° W
6 mins	2025-07-19 22:48:24.185Z	75.539° E	2025-07-19 22:51:24.185Z	49.914° ENE	14.918°	2025-07-19 22:54:24.185Z	24.597° NE

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, 2775 on other resources

View DELTA 1 DEB, 2775 on Heavens-Above

View DELTA 1 DEB, 2775 on Keep Track

View DELTA 1 DEB, 2775 on Celestrak

View DELTA 1 DEB, 2775 on Gunter's Space Page

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