DELTA 1 DEB, 2706

Orbit data source: Space-Track

DELTA 1 DEB, 2706 is space debris in SSO originally from a launch on Thu, 26 Jan 1967 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/2706?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2706, 1967-006C

Orbit

SSO

Last TLE update

2 days ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1967-01-26 (58 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 DELTA 1 DEB
1  2706U 67006C   25198.55081931 -.00000045  00000-0  21991-4 0  9997
2  2706 102.2131 219.7485 0035175 339.6097 171.9821 12.60921089690823

Epoch: 2025-07-17T13:13Z

TLE epoch observation values (Epoch: 2025-07-17T13:13:10.788Z)

Latitude

27.69516°

Longitude

-87.66998°

Altitude

1,449.407 km

Speed

7.127 km/s

True Right ascension

03h 04m 57s

True Declination

27° 33' 59"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

2.3479°

Longitude

-91.49955°

Altitude

1,446.887 km

Speed

7.127 km/s

Apparent Right ascension

01h 29m 29s

Apparent Declination

-49° 09' 12"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:42:06

Azimuth

201.006° SSW

Elevation

-3.752°

Doppler factor

Orbital elements

Apogee altitude

1,444.124 km

Perigee altitude

1,389.287 km

Semi-major axis

7,794.842 km

Eccentricity

0.00352

Inclination

102.2131°

RAAN

219.7485°

Arg. of periapsis

339.6097°

True anomaly

172.03808°

Mean anomaly

171.9821°

Eccentric anomaly

172.01011°

Mean motion

3.15379 °/min

Orbital period

114.15 mins

BSTAR

0.000021991

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Other satellites on launch #6 in the year 1967 (1967-01-26 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.
11 mins	2025-07-19 16:24:57.724Z	352.625° N	2025-07-19 16:30:57.724Z	305.095° NW	19.97°	2025-07-19 16:35:57.724Z	265.957° W
10 mins	2025-07-19 23:37:57.724Z	96.137° ESE	2025-07-19 23:41:57.724Z	59.047° ENE	23.98°	2025-07-19 23:47:57.724Z	6.296° NNE
14 mins	2025-07-20 01:26:57.724Z	170.872° S	2025-07-20 01:33:57.724Z	270.077° WNW	43.48°	2025-07-20 01:40:57.724Z	337.237° NNW
13 mins	2025-07-20 13:25:57.724Z	42.123° NE	2025-07-20 13:31:57.724Z	103.029° ESE	30.37°	2025-07-20 13:38:57.724Z	162.413° S

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, 2706 on other resources

View DELTA 1 DEB, 2706 on Heavens-Above

View DELTA 1 DEB, 2706 on Keep Track

View DELTA 1 DEB, 2706 on Celestrak

View DELTA 1 DEB, 2706 on Gunter's Space Page

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