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 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

10 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, 0.8 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 DELTA 1 R/B
1 03036U 67114B   25199.53229057 -.00000049  00000-0 -13751-4 0  9996
2 03036 102.0153 291.3914 0048252  55.9443 316.0863 12.54132602640526

Epoch: 2025-07-18T12:46Z

TLE epoch observation values (Epoch: 2025-07-18T12:46:29.905Z)

Latitude

11.34618°

Longitude

160.7488°

Altitude

1,421.958 km

Speed

7.163 km/s

True Right ascension

19h 15m 49s

True Declination

11° 17' 08"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

37.309°

Longitude

-7.09494°

Altitude

1,449.716 km

Speed

7.142 km/s

Apparent Right ascension

04h 47m 31s

Apparent Declination

6° 54' 54"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

11:49:36

Azimuth

285.363° WNW

Elevation

-7.267°

Doppler factor

Orbital elements

Apogee altitude

1,482.561 km

Perigee altitude

1,407.067 km

Semi-major axis

7,822.951 km

Eccentricity

0.00483

Inclination

102.0153°

RAAN

291.3914°

Arg. of periapsis

55.9443°

True anomaly

315.70113°

Mean anomaly

316.0863°

Eccentric anomaly

315.89388°

Mean motion

3.1368 °/min

Orbital period

114.77 mins

BSTAR

-0.000013751

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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.
11 mins	2025-07-19 04:12:04.099Z	99.74° ESE	2025-07-19 04:18:04.099Z	48.471° ENE	21.892°	2025-07-19 04:23:04.099Z	7.805° NNE
14 mins	2025-07-19 06:03:04.099Z	167.023° S	2025-07-19 06:09:04.099Z	223.845° SW	44.347°	2025-07-19 06:17:04.099Z	339.778° N
5 mins	2025-07-19 08:01:04.099Z	253.373° W	2025-07-19 08:03:04.099Z	269.044° W	13.248°	2025-07-19 08:06:04.099Z	292.245° WNW
13 mins	2025-07-19 18:05:04.099Z	41.77° NE	2025-07-19 18:11:04.099Z	100.769° ESE	29.68°	2025-07-19 18:18:04.099Z	160.589° S
14 mins	2025-07-19 19:57:04.099Z	5.748° NNE	2025-07-19 20:04:04.099Z	288.208° WNW	38.249°	2025-07-19 20:11:04.099Z	224.346° SW

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, 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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