TIANSHI 01, 68415
Orbit data source: Space-Track
TIANSHI 01, 68415 is a payload satellite owned by Unknown (CN) (CN) in LEO that was launched on Mon, 30 Mar 2026 UTC via a LIJIAN-2 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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68415 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown (CN)
Mission
Operational spacecraft
Bus & Motor
TIANSHI, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.4 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 TIANSHI 01
1 68415U 26066D 26171.51503698 .00001476 00000-0 15424-3 0 9995
2 68415 84.9657 225.6121 0023484 238.7160 121.1764 14.88702330 12227Epoch: 2026-06-20T12:21Z
TLE epoch observation values (Epoch: 2026-06-20T12:21:39.195Z)
Latitude
-0°
Longitude
131.47023°
Altitude
613.609 km
Speed
7.548 km/s
True Right ascension
15h 02m 26s
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
07:18:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
615.297 km
Perigee altitude
582.527 km
Semi-major axis
6,977.049 km
Eccentricity
0.00235
Inclination
84.9657°
RAAN
225.6121°
Arg. of periapsis
238.716°
True anomaly
121.40629°
Mean anomaly
121.1764°
Eccentric anomaly
121.29138°
Mean motion
3.72422 °/min
Orbital period
96.66 mins
BSTAR
0.00015424
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Other satellites on launch #66 in the year 2026 (2026-03-30 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.TIANSHI 01 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 04:38:00.700Z | 209.201° SW | 2026-06-21 04:40:00.700Z | 253.577° W | 37.447° | 2026-06-21 04:44:00.700Z | 351.524° N |
| 4 mins | 2026-06-21 14:46:00.700Z | 47.661° ENE | 2026-06-21 14:48:00.700Z | 85.101° E | 19.225° | 2026-06-21 14:50:00.700Z | 117.604° SE |
| 5 mins | 2026-06-21 16:23:00.700Z | 313.569° NW | 2026-06-21 16:25:00.700Z | 268.257° W | 25.957° | 2026-06-21 16:28:00.700Z | 216.786° SW |
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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