ZY 3 04, 67131
Orbit data source: Space-Track
ZY 3 04, 67131 is a Chinese payload satellite in SSO that was launched on Tue, 16 Dec 2025 UTC via a CHANG ZHENG 4B launch vehicle from the Taiyaun Space Center, China (TSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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67131 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Civil Imaging
Bus & Motor
ZY, AOCS 20N
Mass
2,400 kg wet, ~2,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
10.304 m²
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ZY 3 04
1 67131U 25300A 26094.88964229 .00007548 00000-0 33954-3 0 9998
2 67131 97.4755 173.3256 0007052 197.1462 162.9536 15.21370445 16694Epoch: 2026-04-04T21:21Z
TLE epoch observation values (Epoch: 2026-04-04T21:21:05.093Z)
Latitude
-0.0001°
Longitude
19.85145°
Altitude
509.436 km
Speed
7.607 km/s
True Right ascension
11h 33m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:42:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.522 km
Perigee altitude
493.823 km
Semi-major axis
6,876.81 km
Eccentricity
0.00071
Inclination
97.4755°
RAAN
173.3256°
Arg. of periapsis
197.1462°
True anomaly
162.97727°
Mean anomaly
162.9536°
Eccentric anomaly
162.96544°
Mean motion
3.80595 °/min
Orbital period
94.59 mins
BSTAR
0.00033954
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Other satellites on launch #300 in the year 2025 (2025-12-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ZY 3 04 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 | 2026-04-05 05:22:19.428Z | 177.665° S | 2026-04-05 05:25:19.428Z | 280.701° WNW | 42.319° | 2026-04-05 05:28:19.428Z | 341.316° N |
| 4 mins | 2026-04-05 18:27:19.428Z | 339.041° N | 2026-04-05 18:28:19.428Z | 308.97° NW | 33.149° | 2026-04-05 18:31:19.428Z | 219.927° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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