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

Last TLE update

12 hours ago

Origin

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 (58 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 0.8 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 12 hours ago

0 DELTA 1 R/B
1 03094U 68002B   25199.47986817 -.00000035  00000-0  13800-3 0  9992
2 03094 105.8157  27.2323 0313664 229.4371 188.3267 12.85255804697080

Epoch: 2025-07-18T11:31Z

TLE epoch observation values (Epoch: 2025-07-18T11:31:00.609Z)

Latitude

54.12631°

Longitude

-104.9936°

Altitude

1,568.044 km

Speed

6.978 km/s

True Right ascension

00h 17m 09s

True Declination

53° 58' 46"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

52.14637°

Longitude

119.89219°

Altitude

1,378.434 km

Speed

7.151 km/s

Apparent Right ascension

19h 41m 23s

Apparent Declination

26° 02' 02"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

11:53:03

Azimuth

53.17° ENE

Elevation

-1.842°

Doppler factor

Orbital elements

Apogee altitude

1,559.595 km

Perigee altitude

1,076.783 km

Semi-major axis

7,696.326 km

Eccentricity

0.03137

Inclination

105.8157°

RAAN

27.2323°

Arg. of periapsis

229.4371°

True anomaly

187.82565°

Mean anomaly

188.3267°

Eccentric anomaly

188.07428°

Mean motion

3.21453 °/min

Orbital period

111.99 mins

BSTAR

0.000138

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

EXPLORER 36 (GEOS 2), 3093

DELTA 1 R/B 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.
13 mins	2025-07-19 00:55:29.990Z	36.309° NE	2025-07-19 01:02:29.990Z	98.958° ESE	32.934°	2025-07-19 01:08:29.990Z	168.212° S
12 mins	2025-07-19 02:46:29.990Z	6.475° NNE	2025-07-19 02:52:29.990Z	298.437° NW	35.154°	2025-07-19 02:58:29.990Z	236.614° WSW
9 mins	2025-07-19 09:51:29.990Z	74.975° E	2025-07-19 09:55:29.990Z	45.178° ENE	17.974°	2025-07-19 10:00:29.990Z	7.538° NNE
15 mins	2025-07-19 11:36:29.990Z	139.391° SSE	2025-07-19 11:43:29.990Z	69.342° E	42.598°	2025-07-19 11:51:29.990Z	343.436° N
13 mins	2025-07-19 13:27:29.990Z	206.689° SW	2025-07-19 13:33:29.990Z	259.491° W	27.295°	2025-07-19 13:40:29.990Z	315.734° NNW

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.