CZ-2D R/B, 58074

Orbit data source: Space-Track

CZ-2D R/B, 58074 is space debris in SSO originally from a launch on Sun, 15 Oct 2023 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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/58074?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

58074, 2023-159B

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

BWYIC

Mission

Spacecraft

Bus & Motor

CZ-2 STAGE 2, Unknown motor

Mass

4,006 kg wet, 4,006 kg dry

Launch date (UTC)

2023-10-15 (3 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 4.5 m

Radar Cross Section

27.824 m², Large (>1 m²)

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

TLE from 2 days ago

0 CZ-2D R/B
1 58074U 23159B   26171.44363955  .00000065  00000-0  40465-4 0  9994
2 58074  98.4562 184.1230 0097784 280.0271  78.9888 14.29288829139873

Epoch: 2026-06-20T10:38Z

TLE epoch observation values (Epoch: 2026-06-20T10:38:50.457Z)

Latitude

-0.00008°

Longitude

115.75459°

Altitude

784.309 km

Speed

7.468 km/s

True Right ascension

12h 16m 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

00:25:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

861.348 km

Perigee altitude

721.138 km

Semi-major axis

7,169.38 km

Eccentricity

0.00978

Inclination

98.4562°

RAAN

184.123°

Arg. of periapsis

280.0271°

True anomaly

80.0912°

Mean anomaly

78.9888°

Eccentric anomaly

79.53975°

Mean motion

3.57537 °/min

Orbital period

100.69 mins

BSTAR

0.000040465

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Other satellites on launch #159 in the year 2023 (2023-10-15 UTC)

YUNHAI 1-04, 58073

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CZ-2D R/B 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.
10 mins	2026-06-22 13:37:35.293Z	16.449° NNE	2026-06-22 13:42:35.293Z	83.576° E	44.203°	2026-06-22 13:47:35.293Z	188.669° SSW
4 mins	2026-06-22 23:19:35.293Z	78.647° E	2026-06-22 23:21:35.293Z	54.569° ENE	13.906°	2026-06-22 23:23:35.293Z	32.248° NE
8 mins	2026-06-23 00:56:35.293Z	171.977° S	2026-06-23 00:59:35.293Z	207.589° SW	43.946°	2026-06-23 01:04:35.293Z	343.699° N
8 mins	2026-06-23 13:10:35.293Z	34.765° NE	2026-06-23 13:14:35.293Z	105.98° ESE	33.745°	2026-06-23 13:18:35.293Z	165.052° S

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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 CZ-2D R/B, 58074 on other resources

View CZ-2D R/B, 58074 on Heavens-Above

View CZ-2D R/B, 58074 on Keep Track

View CZ-2D R/B, 58074 on Celestrak

View CZ-2D R/B, 58074 on Gunter's Space Page

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

CZ-2D R/B, 58074

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: 2026-06-20T10:38:50.457Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #159 in the year 2023 (2023-10-15 UTC)

CZ-2D R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2D R/B, 58074 on other resources

Documentation

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