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, 5.0 m
Radar Cross Section
10.304 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ZY 3 04
1 67131U 25300A 26291.62566361 .00004451 00000-0 20179-3 0 9999
2 67131 97.4636 8.5354 0005851 236.7491 123.3184 15.21345613 46600Epoch: 2026-10-18T15:00Z
TLE epoch observation values (Epoch: 2026-10-18T15:00:57.335Z)
Latitude
-0.00009°
Longitude
116.18124°
Altitude
507.085 km
Speed
7.609 km/s
True Right ascension
00h 34m 08s
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
20:32:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.771 km
Perigee altitude
494.724 km
Semi-major axis
6,876.884 km
Eccentricity
0.00059
Inclination
97.4636°
RAAN
8.5354°
Arg. of periapsis
236.7491°
True anomaly
123.3744°
Mean anomaly
123.3184°
Eccentric anomaly
123.3464°
Mean motion
3.80588 °/min
Orbital period
94.59 mins
BSTAR
0.00020179
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-19 05:20:14.129Z | 169.441° S | 2026-10-19 05:24:14.129Z | 325.074° NNW | 72.294° | 2026-10-19 05:27:14.129Z | 346.132° N |
| 5 mins | 2026-10-19 18:25:14.129Z | 356.468° N | 2026-10-19 18:27:14.129Z | 312.43° NW | 49.774° | 2026-10-19 18:30:14.129Z | 212.732° 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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