TIANPING 3A-01, 61614
Orbit data source: Space-Track
TIANPING 3A-01, 61614 is a payload satellite owned by ZJUNI-SAT (CN) in SSO that was launched on Tue, 22 Oct 2024 UTC via a CHANG ZHENG 6 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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61614 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
ZJUNI-SAT
Mission
Operational Defense Calibration
Bus & Motor
TP-3, Unknown motor
Mass
200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.135 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 TIANPING 3A-01
1 61614U 24189A 25311.18951900 .00004774 00000-0 37901-3 0 9992
2 61614 97.5519 333.0815 0002450 93.7305 266.4200 15.00943212 57185Epoch: 2025-11-07T04:32Z
TLE epoch observation values (Epoch: 2025-11-07T04:32:54.441Z)
Latitude
0.00002°
Longitude
-141.78239°
Altitude
567.153 km
Speed
7.577 km/s
True Right ascension
22h 12m 19s
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
08:01:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.684 km
Perigee altitude
559.284 km
Semi-major axis
6,939.121 km
Eccentricity
0.00025
Inclination
97.5519°
RAAN
333.0815°
Arg. of periapsis
93.7305°
True anomaly
266.39198°
Mean anomaly
266.42°
Eccentric anomaly
266.40599°
Mean motion
3.7548 °/min
Orbital period
95.88 mins
BSTAR
0.00037901
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Other satellites on launch #189 in the year 2024 (2024-10-22 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.TIANPING 3A-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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-07 14:42:02.298Z | 4.2° NNE | 2025-11-07 14:46:02.298Z | 276.18° WNW | 40.692° | 2025-11-07 14:49:02.298Z | 208.128° SW |
| 6 mins | 2025-11-08 01:29:02.298Z | 156.032° SSE | 2025-11-08 01:32:02.298Z | 41.546° NE | 42.379° | 2025-11-08 01:35:02.298Z | 354.053° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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