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 25256.99147756 .00003008 00000-0 23995-3 0 9992
2 61614 97.5625 280.3639 0002704 101.4266 258.7262 15.01042475 49057Epoch: 2025-09-13T23:47Z
TLE epoch observation values (Epoch: 2025-09-13T23:47:43.661Z)
Latitude
-0.00002°
Longitude
-69.78491°
Altitude
567.108 km
Speed
7.577 km/s
True Right ascension
18h 41m 27s
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
23:27:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.555 km
Perigee altitude
558.802 km
Semi-major axis
6,938.815 km
Eccentricity
0.00027
Inclination
97.5625°
RAAN
280.3639°
Arg. of periapsis
101.4266°
True anomaly
258.69581°
Mean anomaly
258.7262°
Eccentric anomaly
258.71101°
Mean motion
3.75505 °/min
Orbital period
95.87 mins
BSTAR
0.00023995
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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 | 2025-09-14 14:45:21.582Z | 2.644° NNE | 2025-09-14 14:48:21.582Z | 309.912° NW | 40.035° | 2025-09-14 14:52:21.582Z | 206.196° SW |
| 6 mins | 2025-09-15 01:32:21.582Z | 153.342° SSE | 2025-09-15 01:34:21.582Z | 87.002° E | 43.08° | 2025-09-15 01:38:21.582Z | 352.974° N |
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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