DELTA 2 R/B(2), 22177

Orbit data source: Space-Track

DELTA 2 R/B(2), 22177 is space debris in HEO originally from a launch on Mon, 12 Oct 1992 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.

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https://www.satcat.com/sats-embedded/22177?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22177, 1992-066C

Orbit

HEO

Last TLE update

3 days ago

Origin

MDA Inc. (US)

Manufacturer

Thiokol/TE

Mission

Spacecraft

Bus & Motor

STAR 48, Unknown motor

Mass

133 kg wet, 132 kg dry

Launch date (UTC)

1992-10-12 (33 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Sphere + Cone, 2.3 m

Radar Cross Section

2.822 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 days ago

0 DELTA 2 R/B(2)
1 22177U 92066C   25120.59939347 -.00000143  00000-0  00000-0 0  9990
2 22177  19.1074 227.4194 6843641 354.9957  15.3697  2.18728682 40689

Epoch: 2025-04-30T14:23Z

Definitive object data (Epoch: 2025-04-30T14:23:07.595Z)

Latitude

18.72933°

Longitude

-130.72077°

Altitude

5,779.551 km

Speed

7.048 km/s

True Right ascension

20h 15m 22s

True Declination

18° 40' 05"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-4.66135°

Longitude

-14.30547°

Altitude

31,800.824 km

Speed

2.232 km/s

Apparent Right ascension

03h 37m 05s

Apparent Declination

-9° 59' 12"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:00:45

Azimuth

286.593° WNW

Elevation

-33.666°

Doppler factor

Orbital elements

Apogee altitude

35,853.07 km

Perigee altitude

1,535.642 km

Semi-major axis

25,072.493 km

Eccentricity

0.6843641

Inclination

19.1074°

RAAN

227.4194°

Arg. of periapsis

354.9957°

True anomaly

81.92824°

Mean anomaly

15.3697°

Eccentric anomaly

41.19523°

Mean motion

0.5467 °/min

BSTAR

Unknown

Orbital period

658.5 mins

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Other satellites on launch #66 in the year 1992 (1992-10-12 UTC)

HELLAS-SAT 1 (DFS 3), 22175

DELTA 2 R/B(1), 22176

DELTA 2 R/B(2) 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.
187 mins	2025-05-03 19:54:55.816Z	269.021° W	2025-05-03 21:00:55.816Z	258.991° W	17.902°	2025-05-03 23:01:55.816Z	259.386° W

Authenticating...

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Check out DELTA 2 R/B(2), 22177 on other resources

View DELTA 2 R/B(2), 22177 on Heavens-Above

View DELTA 2 R/B(2), 22177 on Keep Track

View DELTA 2 R/B(2), 22177 on Celestrak

View DELTA 2 R/B(2), 22177 on Gunter's Space Page

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