DELTA 1 R/B, 3094

Orbit data source: Space-Track

DELTA 1 R/B, 3094 is space debris in LEO originally from a launch on Thu, 11 Jan 1968 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/3094?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

3094, 1968-002B

Orbit

LEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

UTC

Mission

Spacecraft

Bus & Motor

FW4, Unknown motor

Mass

~40 kg wet, ~40 kg dry

Launch date (UTC)

1968-01-11 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

CYL, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago

0 DELTA 1 R/B
1 03094U 68002B   26316.09328953 -.00000044  00000-0  10495-3 0  9990
2 03094 105.8103 344.6836 0313228 166.0818 213.0656 12.85293790758963

Epoch: 2026-11-12T02:14Z

TLE epoch observation values (Epoch: 2026-11-12T02:14:20.215Z)

Latitude

16.57001°

Longitude

-104.94201°

Altitude

1,526.345 km

Speed

7.009 km/s

True Right ascension

22h 39m 29s

True Declination

16° 29' 07"

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

17:15:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,559.103 km

Perigee altitude

1,076.972 km

Semi-major axis

7,696.174 km

Eccentricity

0.03132

Inclination

105.8103°

RAAN

344.6836°

Arg. of periapsis

166.0818°

True anomaly

211.1699°

Mean anomaly

213.0656°

Eccentric anomaly

212.11161°

Mean motion

3.21463 °/min

Orbital period

111.99 mins

BSTAR

0.00010495

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Other satellites on launch #2 in the year 1968 (1968-01-11 UTC)

EXPLORER 36 (GEOS 2), 3093

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DELTA 1 R/B 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.
13 mins	2026-11-13 00:42:34.279Z	122.621° SE	2026-11-13 00:48:34.279Z	61.326° ENE	47.05°	2026-11-13 00:55:34.279Z	350.093° N
14 mins	2026-11-13 02:31:34.279Z	189.637° SSW	2026-11-13 02:37:34.279Z	245.086° WSW	42.795°	2026-11-13 02:45:34.279Z	323.439° NNW
9 mins	2026-11-13 14:18:34.279Z	54.649° ENE	2026-11-13 14:22:34.279Z	103.22° ESE	29.053°	2026-11-13 14:27:34.279Z	158.667° S
10 mins	2026-11-13 16:07:34.279Z	6.784° NNE	2026-11-13 16:12:34.279Z	294.48° NW	48.245°	2026-11-13 16:17:34.279Z	231.876° WSW

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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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Check out DELTA 1 R/B, 3094 on other resources

View DELTA 1 R/B, 3094 on Heavens-Above

View DELTA 1 R/B, 3094 on Keep Track

View DELTA 1 R/B, 3094 on Celestrak

View DELTA 1 R/B, 3094 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 R/B, 3094

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-11-12T02:14:20.215Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #2 in the year 1968 (1968-01-11 UTC)

DELTA 1 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 R/B, 3094 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago