DAQI-2, 68760
Orbit data source: Space-Track
DAQI-2, 68760 is a payload satellite owned by CRESDA (CN) in SSO that was launched on Fri, 17 Apr 2026 UTC via a CHANG ZHENG 4C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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68760 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational spacecraft
Bus & Motor
ZY, AOCS 20N
Mass
2,640 kg wet, ~2,300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 DAQI-2
1 68760U 26084A 26138.85863420 .00000012 00000-0 12802-4 0 9993
2 68760 98.2868 213.1499 0002203 152.1223 208.0094 14.57608565 4624Epoch: 2026-05-18T20:36Z
TLE epoch observation values (Epoch: 2026-05-18T20:36:25.994Z)
Latitude
-0.00004°
Longitude
27.50074°
Altitude
705.263 km
Speed
7.502 km/s
True Right ascension
14h 12m 35s
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
10:14:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.554 km
Perigee altitude
696.436 km
Semi-major axis
7,076.132 km
Eccentricity
0.00022
Inclination
98.2868°
RAAN
213.1499°
Arg. of periapsis
152.1223°
True anomaly
207.99755°
Mean anomaly
208.0094°
Eccentric anomaly
208.00347°
Mean motion
3.64627 °/min
Orbital period
98.73 mins
BSTAR
0.000012802
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Other satellites on launch #84 in the year 2026 (2026-04-17 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.DAQI-2 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-19 04:58:16.727Z | 168.461° S | 2026-05-19 05:01:16.727Z | 184.149° SSW | 43.752° | 2026-05-19 05:06:16.727Z | 345.779° N |
| 5 mins | 2026-05-19 16:59:16.727Z | 57.464° ENE | 2026-05-19 17:01:16.727Z | 92.882° ESE | 23.019° | 2026-05-19 17:04:16.727Z | 142.244° SSE |
| 6 mins | 2026-05-19 18:36:16.727Z | 342.549° N | 2026-05-19 18:39:16.727Z | 285.953° WNW | 27.723° | 2026-05-19 18:42:16.727Z | 235.705° WSW |
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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