OPS 5798 DEB, 901

Orbit data source: Space-Track

OPS 5798 DEB, 901 is space debris in LEO originally from a launch on Tue, 06 Oct 1964 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/901?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/901?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

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ISO8601 Format

Identifier

901, 1964-063D

Orbit

LEO

Last TLE update

1 day ago

Origin

United States Navy (US)

Manufacturer

NAFI?

Mission

Spacecraft

Bus & Motor

Unknown

Mass

~20 kg wet, ~20 kg dry

Launch date (UTC)

1964-10-06 (61 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

1.300 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 OPS 5798 DEB
1 00901U 64063D   25181.77284072  .00000091  00000-0  11893-3 0  9998
2 00901  90.2319  68.1353 0021277  67.8401   2.1144 13.55067223998863

Epoch: 2025-06-30T18:32Z

TLE epoch observation values (Epoch: 2025-06-30T18:32:53.438Z)

Latitude

70.03258°

Longitude

-129.8002°

Altitude

1,050.067 km

Speed

7.341 km/s

True Right ascension

04h 30m 00s

True Declination

69° 55' 35"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

3.53024°

Longitude

50.87218°

Altitude

1,061.986 km

Speed

7.318 km/s

Apparent Right ascension

17h 01m 52s

Apparent Declination

-16° 32' 28"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

05:46:16

Azimuth

25.597° NE

Elevation

-64.712°

Doppler factor

Orbital elements

Apogee altitude

1,066.522 km

Perigee altitude

1,034.909 km

Semi-major axis

7,428.853 km

Eccentricity

0.00213

Inclination

90.2319°

RAAN

68.1353°

Arg. of periapsis

67.8401°

True anomaly

Unknown

Mean anomaly

2.1144°

Eccentric anomaly

Unknown

Mean motion

3.38969 °/min

Orbital period

106.2 mins

BSTAR

0.00011893

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Other satellites on launch #63 in the year 1964 (1964-10-06 UTC)

THOR ABLESTAR R/B, 893

OPS 5798 (TRANSIT 5B-4), 897

CALSPHERE 1, 900

CALSPHERE 2, 902

OPS 5798 DEB, 903

OPS 5798 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.
12 mins	2025-07-02 04:27:33.838Z	8.324° NNE	2025-07-02 04:33:33.838Z	74.188° E	42.312°	2025-07-02 04:39:33.838Z	171.584° S
7 mins	2025-07-02 06:16:33.838Z	317.069° NNW	2025-07-02 06:19:33.838Z	284.107° WNW	18.146°	2025-07-02 06:23:33.838Z	245.764° WSW
11 mins	2025-07-02 16:23:33.838Z	160.851° S	2025-07-02 16:28:33.838Z	93.294° ESE	41.945°	2025-07-02 16:34:33.838Z	4.773° NNE

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Check out OPS 5798 DEB, 901 on other resources

View OPS 5798 DEB, 901 on Heavens-Above

View OPS 5798 DEB, 901 on Keep Track

View OPS 5798 DEB, 901 on Celestrak

View OPS 5798 DEB, 901 on Gunter's Space Page

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