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 src="https://www.satcat.com/sats-embedded/3094?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

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

1 day 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 (57 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.5 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 day ago

0 DELTA 1 R/B
1 03094U 68002B   25181.34737715 -.00000062  00000-0  49403-4 0  9999
2 03094 105.8150   1.7153 0313723 258.8710 170.8029 12.85254516694752

Epoch: 2025-06-30T08:20Z

TLE epoch observation values (Epoch: 2025-06-30T08:20:13.385Z)

Latitude

64.96834°

Longitude

-79.13016°

Altitude

1,569.901 km

Speed

6.978 km/s

True Right ascension

21h 38m 20s

True Declination

64° 50' 59"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

35.58°

Longitude

151.08077°

Altitude

1,417.916 km

Speed

7.112 km/s

Apparent Right ascension

11h 07m 58s

Apparent Declination

2° 40' 27"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:39:17

Azimuth

312.16° NW

Elevation

-35.489°

Doppler factor

Orbital elements

Apogee altitude

1,559.646 km

Perigee altitude

1,076.743 km

Semi-major axis

7,696.332 km

Eccentricity

0.03137

Inclination

105.815°

RAAN

1.7153°

Arg. of periapsis

258.871°

True anomaly

Unknown

Mean anomaly

170.8029°

Eccentric anomaly

Unknown

Mean motion

3.21453 °/min

Orbital period

111.99 mins

BSTAR

0.000049403

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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.
14 mins	2025-07-01 10:16:04.353Z	110.292° ESE	2025-07-01 10:22:04.353Z	58.444° ENE	30.511°	2025-07-01 10:30:04.353Z	351.749° N
15 mins	2025-07-01 12:05:04.353Z	175.464° S	2025-07-01 12:11:04.353Z	241.919° WSW	41.312°	2025-07-01 12:20:04.353Z	331.195° NNW
10 mins	2025-07-01 23:53:04.353Z	56.822° ENE	2025-07-01 23:58:04.353Z	102.012° ESE	22.655°	2025-07-02 00:03:04.353Z	145.982° SSE
14 mins	2025-07-02 01:41:04.353Z	17.698° NNE	2025-07-02 01:48:04.353Z	283.166° WNW	43.704°	2025-07-02 01:55:04.353Z	214.918° SW
9 mins	2025-07-02 03:32:04.353Z	347.652° N	2025-07-02 03:36:04.353Z	314.912° NW	18.707°	2025-07-02 03:41:04.353Z	276.435° WNW
4 mins	2025-07-02 08:50:04.353Z	46.568° ENE	2025-07-02 08:52:04.353Z	32.6° NE	11.965°	2025-07-02 08:54:04.353Z	18.838° NNE

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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

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