P/L 153 DEB, 19245

Orbit data source: Space-Track

P/L 153 DEB, 19245 is space debris in LEO originally from a launch on Wed, 31 May 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/19245?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

19245, 1967-053K

Orbit

LEO

Last TLE update

8 hours ago

Origin

United States Navy (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1967-05-31 (58 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 8 hours ago

0 P/L 153 DEB
1 19245U 67053K   25182.06713314  .00000350  00000-0  18269-3 0  9992
2 19245  69.9575  44.0272 0005747 252.2175 226.2568 14.22352919980635

Epoch: 2025-07-01T01:36Z

TLE epoch observation values (Epoch: 2025-07-01T01:36:40.303Z)

Latitude

55.82042°

Longitude

-111.80994°

Altitude

828.946 km

Speed

7.443 km/s

True Right ascension

12h 46m 54s

True Declination

55° 39' 43"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

12.00732°

Longitude

104.17758°

Altitude

821.116 km

Speed

7.443 km/s

Apparent Right ascension

05h 30m 22s

Apparent Declination

-16° 46' 22"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:11:34

Azimuth

80.735° E

Elevation

-37.101°

Doppler factor

Orbital elements

Apogee altitude

819.563 km

Perigee altitude

811.295 km

Semi-major axis

7,193.566 km

Eccentricity

0.00057

Inclination

69.9575°

RAAN

44.0272°

Arg. of periapsis

252.2175°

True anomaly

Unknown

Mean anomaly

226.2568°

Eccentric anomaly

Unknown

Mean motion

3.55735 °/min

Orbital period

101.2 mins

BSTAR

0.00018269

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Other satellites on launch #53 in the year 1967 (1967-05-31 UTC)

OPS 5712 (P/L 160), 2826

THOR AGENA D R/B, 2825

OPS 5712 (P/L 152), 2873

OPS 5712 (P/L 153), 2874

SURCAL 150B, 2909

P/L 153 DEB, 39247 (Decayed)

P/L 153 DEB 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.
9 mins	2025-07-01 16:23:16.490Z	207.614° SW	2025-07-01 16:27:16.490Z	346.341° N	44.389°	2025-07-01 16:32:16.490Z	22.914° NE
8 mins	2025-07-02 01:15:16.490Z	356.339° N	2025-07-02 01:18:16.490Z	45.709° ENE	34.956°	2025-07-02 01:23:16.490Z	130.033° SE
7 mins	2025-07-02 02:59:16.490Z	295.745° NW	2025-07-02 03:02:16.490Z	253.014° W	21.835°	2025-07-02 03:06:16.490Z	205.787° SW

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Check out P/L 153 DEB, 19245 on other resources

View P/L 153 DEB, 19245 on Heavens-Above

View P/L 153 DEB, 19245 on Keep Track

View P/L 153 DEB, 19245 on Celestrak

View P/L 153 DEB, 19245 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.