YAOGAN-50 02 DEB, 100580

Orbit data source: Space-Track

YAOGAN-50 02 DEB, 100580 is space debris in LEO originally from a launch on Sun, 15 Mar 2026 UTC launched from the Taiyaun Space Center, China (TSC). 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/100580?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

100580, 2026-051U

Orbit

LEO

Country

CN / PRC

Related business

Zhongguo Weixing Wangluo Jituan YG (CN)

Manufacturer

CAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2026-03-15 (6 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 YAOGAN-50 02 DEB
1 A0580U 26051U   26260.30494128  .00036278  00000-0  11997-1 0  9998
2 A0580 141.9211  66.3741 0297442  79.4176 283.9921 14.14554094  7450

Epoch: 2026-09-17T07:19Z

TLE epoch observation values (Epoch: 2026-09-17T07:19:06.926Z)

Latitude

0.00001°

Longitude

-39.64887°

Altitude

797.249 km

Speed

7.48 km/s

True Right ascension

04h 25m 29s

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

04:11:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,061.347 km

Perigee altitude

631.567 km

Semi-major axis

7,224.594 km

Eccentricity

0.02974

Inclination

141.9211°

RAAN

66.3741°

Arg. of periapsis

79.4176°

True anomaly

280.65669°

Mean anomaly

283.9921°

Eccentric anomaly

282.32717°

Mean motion

3.53446 °/min

Orbital period

101.85 mins

BSTAR

0.011997

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Other satellites on launch #51 in the year 2026 (2026-03-15 UTC)

YAOGAN-50 02, 68196

YAOGAN-50 02 DEB, 100590

YAOGAN-50 02 DEB, 100570

YAOGAN-50 02 DEB, 100585

YAOGAN-50 02 DEB, 100593

YAOGAN-50 02 DEB, 100594

YAOGAN-50 02 DEB, 100597

YAOGAN-50 02 DEB, 100601

YAOGAN-50 02 DEB, 100599

YAOGAN-50 02 DEB, 100604

YAOGAN-50 02 DEB, 100573

YAOGAN-50 02 DEB, 100571

YAOGAN-50 02 DEB, 100605

YAOGAN-50 02 DEB, 100606

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YAOGAN-50 02 DEB Visibility forecast

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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.
6 mins	2026-09-20 03:35:37.918Z	104.407° ESE	2026-09-20 03:38:37.918Z	162.075° S	27.54°	2026-09-20 03:41:37.918Z	212.373° SW
6 mins	2026-09-20 05:12:37.918Z	94.654° ESE	2026-09-20 05:15:37.918Z	189.189° SSW	57.259°	2026-09-20 05:18:37.918Z	246.681° WSW
6 mins	2026-09-20 06:49:37.918Z	103.163° ESE	2026-09-20 06:51:37.918Z	135.642° SSE	62.542°	2026-09-20 06:55:37.918Z	266.482° W
6 mins	2026-09-20 08:26:37.918Z	136.254° SSE	2026-09-20 08:28:37.918Z	183.519° SSW	44.002°	2026-09-20 08:32:37.918Z	268.058° W
5 mins	2026-09-20 10:03:37.918Z	173.35° S	2026-09-20 10:05:37.918Z	203.356° SW	18.566°	2026-09-20 10:08:37.918Z	248.94° W

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

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Check out YAOGAN-50 02 DEB, 100580 on other resources

View YAOGAN-50 02 DEB, 100580 on Heavens-Above

View YAOGAN-50 02 DEB, 100580 on Keep Track

View YAOGAN-50 02 DEB, 100580 on Celestrak

View YAOGAN-50 02 DEB, 100580 on Gunter's Space Page

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

YAOGAN-50 02 DEB, 100580

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-09-17T07:19:06.926Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #51 in the year 2026 (2026-03-15 UTC)

YAOGAN-50 02 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out YAOGAN-50 02 DEB, 100580 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago