**DELTA 1 R/B(2) *, 11792**

Orbit data source: Space-Track

DELTA 1 R/B(2) *, 11792 is space debris in HEO originally from a launch on Wed, 26 Oct 1966 UTC launched from the Air Force Eastern Test Range (AFETR). 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.

Loading next visibility...

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/11792?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/11792?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

11792, 1966-096C

Orbit

HEO

Country

Related business

European Space Agency (FR)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-10-26 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 DELTA 1 R/B(2) *
1 11792U 66096C   25349.01659653  .00006738  00000-0  66685-2 0  9992
2 11792  17.7148 194.1471 6075784  23.6058 355.4122  3.83194661424304

Epoch: 2025-12-15T00:23Z

TLE epoch observation values (Epoch: 2025-12-15T00:23:53.940Z)

Latitude

-0.00007°

Longitude

104.25456°

Altitude

609.008 km

Speed

9.538 km/s

True Right ascension

12h 56m 36s

True Declination

0° 00' 00"

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

00:56:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

21,359.648 km

Perigee altitude

392.858 km

Semi-major axis

17,254.39 km

Eccentricity

0.60758

Inclination

17.7148°

RAAN

194.1471°

Arg. of periapsis

23.6058°

True anomaly

336.82469°

Mean anomaly

355.4122°

Eccentric anomaly

348.43048°

Mean motion

0.95762 °/min

Orbital period

375.93 mins

BSTAR

0.0066685

Loading maneuver chart data...

Computing Atmospheric mass density...

Loading historical data...

Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

DELTA 1 R/B(1), 2515 (Decayed)

INTELSAT 2-F1, 2514

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

DELTA 1 R/B(2) * Visibility forecast

Loading observer location...
Set Observer location

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.
274 mins	2025-12-16 02:17:24.735Z	239.256° WSW	2025-12-16 03:10:24.735Z	208.347° SW	29.728°	2025-12-16 06:51:24.735Z	170.103° S
69 mins	2025-12-16 20:32:24.735Z	210.523° SW	2025-12-16 20:40:24.735Z	159.094° S	28.442°	2025-12-16 21:41:24.735Z	110.595° ESE

Items per page:

1–2 of 2 items

of 1 page

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Please sign-in to view Co-orbital & Co-planar RSOs.

Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in descending order

CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in descending order

Check out DELTA 1 R/B(2) *, 11792 on other resources

View DELTA 1 R/B(2) *, 11792 on Heavens-Above

View DELTA 1 R/B(2) *, 11792 on Keep Track

View DELTA 1 R/B(2) *, 11792 on Celestrak

View DELTA 1 R/B(2) *, 11792 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(2) *, 11792

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-15T00:23:53.940Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

DELTA 1 R/B(2) * Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 R/B(2) *, 11792 on other resources

Documentation

**DELTA 1 R/B(2) *, 11792**

Expand to show TLE details & history
Last TLE update: 1 day ago