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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 DAQI-2
1 68760U 26084A 26171.53516248 .00000018 00000-0 14215-4 0 9994
2 68760 98.2862 245.6880 0003400 93.6813 266.4774 14.57576841 9388Epoch: 2026-06-20T12:50Z
TLE epoch observation values (Epoch: 2026-06-20T12:50:38.038Z)
Latitude
-0.00004°
Longitude
144.28112°
Altitude
704.137 km
Speed
7.504 km/s
True Right ascension
16h 22m 45s
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
07:24:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
700.503 km
Perigee altitude
695.691 km
Semi-major axis
7,076.234 km
Eccentricity
0.00034
Inclination
98.2862°
RAAN
245.688°
Arg. of periapsis
93.6813°
True anomaly
266.43851°
Mean anomaly
266.4774°
Eccentric anomaly
266.45796°
Mean motion
3.64619 °/min
Orbital period
98.73 mins
BSTAR
0.000014215
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 03:49:36.342Z | 106.467° ESE | 2026-06-21 03:52:36.342Z | 64.12° ENE | 18.247° | 2026-06-21 03:55:36.342Z | 22.634° NE |
| 7 mins | 2026-06-21 05:26:36.342Z | 194.873° SSW | 2026-06-21 05:29:36.342Z | 249.456° W | 34.425° | 2026-06-21 05:33:36.342Z | 329.41° NNW |
| 7 mins | 2026-06-21 17:26:36.342Z | 32.772° NE | 2026-06-21 17:29:36.342Z | 96.293° ESE | 36.293° | 2026-06-21 17:33:36.342Z | 171.286° S |
| 4 mins | 2026-06-21 19:05:36.342Z | 317.286° NNW | 2026-06-21 19:06:36.342Z | 301.976° NW | 17.061° | 2026-06-21 19:09:36.342Z | 258.724° W |
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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