DELTA 1 DEB, 10626

Orbit data source: Space-Track

DELTA 1 DEB, 10626 is space debris in LEO originally from a launch on Thu, 14 Jul 1977 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/10626?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

10626, 1977-065EV

Orbit

LEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1977-07-14 (48 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

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: 14 hours ago

TLE from 14 hours ago

0 DELTA 1 DEB
1 10626U 77065EV  25350.33375986  .00001052  00000-0  23461-3 0  9996
2 10626  29.1749   4.6548 0659100 138.4630 226.7969 13.67165568357567

Epoch: 2025-12-16T08:00Z

TLE epoch observation values (Epoch: 2025-12-16T08:00:36.851Z)

Latitude

-0.00001°

Longitude

159.28177°

Altitude

1,357.408 km

Speed

7.01 km/s

True Right ascension

00h 18m 37s

True Declination

0° 00' 00"

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

20:57:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,500.824 km

Perigee altitude

526.441 km

Semi-major axis

7,391.769 km

Eccentricity

0.06591

Inclination

29.1749°

RAAN

4.6548°

Arg. of periapsis

138.463°

True anomaly

221.5931°

Mean anomaly

226.7969°

Eccentric anomaly

224.16577°

Mean motion

3.41523 °/min

Orbital period

105.41 mins

BSTAR

0.00023461

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Other satellites on launch #65 in the year 1977 (1977-07-14 UTC)

DELTA 1 DEB, 10182 (Decayed)

DELTA 1 DEB, 10191 (Decayed)

DELTA 1 DEB, 10473 (Decayed)

DELTA 1 DEB, 10310 (Decayed)

DELTA 1 DEB, 10268 (Decayed)

DELTA 1 DEB, 10226 (Decayed)

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DELTA 1 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.
4 mins	2025-12-17 03:28:59.534Z	175.687° S	2025-12-17 03:30:59.534Z	159.185° S	12.048°	2025-12-17 03:32:59.534Z	141.378° SSE
7 mins	2025-12-17 05:18:59.534Z	209.922° SW	2025-12-17 05:22:59.534Z	164.227° S	20.612°	2025-12-17 05:25:59.534Z	127.024° SE
6 mins	2025-12-17 07:10:59.534Z	225.03° WSW	2025-12-17 07:13:59.534Z	181.337° SSW	22.447°	2025-12-17 07:16:59.534Z	135.704° SSE

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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 DELTA 1 DEB, 10626 on other resources

View DELTA 1 DEB, 10626 on Heavens-Above

View DELTA 1 DEB, 10626 on Keep Track

View DELTA 1 DEB, 10626 on Celestrak

View DELTA 1 DEB, 10626 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

DELTA 1 DEB, 10626

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2025-12-16T08:00:36.851Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #65 in the year 1977 (1977-07-14 UTC)

DELTA 1 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB, 10626 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago