CZ-3B R/B, 59070

Orbit data source: Space-Track

CZ-3B R/B, 59070 is space debris in HEO originally from a launch on Thu, 29 Feb 2024 UTC launched from the Xichang Space Center, China (XSC). 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/59070?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59070, 2024-040B

Orbit

HEO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

~2,800 kg wet, ~2,800 kg dry

Launch date (UTC)

2024-02-29 (2 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 6.2 m

Radar Cross Section

32.704 m², Large (>1 m²)

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

TLE from 2 days ago

0 CZ-3B R/B
1 59070U 24040B   26171.38853666  .00197372 -10160-6  26535-2 0  9990
2 59070  27.3504 293.9638 6466744 150.1392 272.0248  3.44475337 24036

Epoch: 2026-06-20T09:19Z

TLE epoch observation values (Epoch: 2026-06-20T09:19:29.567Z)

Latitude

0.00003°

Longitude

-114.53288°

Altitude

18,147.699 km

Speed

3.314 km/s

True Right ascension

19h 35m 46s

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

21:31:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

24,123.534 km

Perigee altitude

166.582 km

Semi-major axis

18,523.195 km

Eccentricity

0.64667

Inclination

27.3504°

RAAN

293.9638°

Arg. of periapsis

150.1392°

True anomaly

209.91794°

Mean anomaly

272.0248°

Eccentric anomaly

239.95246°

Mean motion

0.86093 °/min

Orbital period

418.15 mins

BSTAR

0.0026535

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Other satellites on launch #40 in the year 2024 (2024-02-29 UTC)

HG-01, 59069

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CZ-3B 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.
58 mins	2026-06-22 10:29:56.222Z	209.896° SW	2026-06-22 11:09:56.222Z	171.01° S	38.211°	2026-06-22 11:27:56.222Z	101.073° ESE
274 mins	2026-06-23 03:28:56.222Z	156.011° SSE	2026-06-23 07:11:56.222Z	137.155° SSE	28.649°	2026-06-23 08:02:56.222Z	96.231° ESE

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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-3B R/B, 59070 on other resources

View CZ-3B R/B, 59070 on Heavens-Above

View CZ-3B R/B, 59070 on Keep Track

View CZ-3B R/B, 59070 on Celestrak

View CZ-3B R/B, 59070 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-3B R/B, 59070

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: 2026-06-20T09:19:29.567Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #40 in the year 2024 (2024-02-29 UTC)

CZ-3B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3B R/B, 59070 on other resources

Documentation

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