DELTA 1 R/B, 3036

Orbit data source: Space-Track

DELTA 1 R/B, 3036 is space debris in SSO originally from a launch on Fri, 10 Nov 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 src="https://www.satcat.com/sats-embedded/3036?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/3036?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

3036, 1967-114B

Orbit

SSO

Last TLE update

14 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)

1967-11-10 (58 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 14 hours ago

0 DELTA 1 R/B
1 03036U 67114B   25191.79206323 -.00000038  00000-0  49333-4 0  9999
2 03036 102.0134 283.5457 0047708  70.4708 290.1508 12.54132454639555

Epoch: 2025-07-10T19:00Z

TLE epoch observation values (Epoch: 2025-07-10T19:00:34.263Z)

Latitude

0.00005°

Longitude

69.44966°

Altitude

1,437.12 km

Speed

7.149 km/s

True Right ascension

18h 54m 10s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

38.42084°

Longitude

-100.28444°

Altitude

1,440.198 km

Speed

7.151 km/s

Apparent Right ascension

08h 24m 40s

Apparent Declination

4° 05' 34"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:26:49

Azimuth

21.702° NNE

Elevation

-43.731°

Doppler factor

Orbital elements

Apogee altitude

1,482.136 km

Perigee altitude

1,407.493 km

Semi-major axis

7,822.951 km

Eccentricity

0.00477

Inclination

102.0134°

RAAN

283.5457°

Arg. of periapsis

70.4708°

True anomaly

Unknown

Mean anomaly

290.1508°

Eccentric anomaly

Unknown

Mean motion

3.1368 °/min

Orbital period

114.77 mins

BSTAR

0.000049333

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Other satellites on launch #114 in the year 1967 (1967-11-10 UTC)

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.
15 mins	2025-07-11 18:36:09.825Z	27.143° NE	2025-07-11 18:43:09.825Z	91.473° ESE	39.525°	2025-07-11 18:51:09.825Z	179.552° S
12 mins	2025-07-11 20:30:09.825Z	355.793° N	2025-07-11 20:36:09.825Z	297.783° NW	28.979°	2025-07-11 20:42:09.825Z	244.895° WSW
7 mins	2025-07-12 03:47:09.825Z	73.306° E	2025-07-12 03:50:09.825Z	48.815° ENE	15.85°	2025-07-12 03:54:09.825Z	17.305° NNE
14 mins	2025-07-12 05:35:09.825Z	149.379° SSE	2025-07-12 05:41:09.825Z	89.125° E	43.644°	2025-07-12 05:49:09.825Z	346.373° N
10 mins	2025-07-12 07:30:09.825Z	225.084° WSW	2025-07-12 07:35:09.825Z	269.11° W	20.934°	2025-07-12 07:40:09.825Z	310.632° NW

Authenticating...

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Check out DELTA 1 R/B, 3036 on other resources

View DELTA 1 R/B, 3036 on Heavens-Above

View DELTA 1 R/B, 3036 on Keep Track

View DELTA 1 R/B, 3036 on Celestrak

View DELTA 1 R/B, 3036 on Gunter's Space Page

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