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: 2 days ago
TLE from 2 days ago
0 TIANPING 3A-01
1 61614U 24189A 25258.99133116 .00004013 00000-0 31839-3 0 9992
2 61614 97.5626 282.3106 0002804 99.7536 260.4006 15.01057869 49351Epoch: 2025-09-15T23:47Z
TLE epoch observation values (Epoch: 2025-09-15T23:47:31.012Z)
Latitude
0.00008°
Longitude
-69.75667°
Altitude
567.018 km
Speed
7.577 km/s
True Right ascension
18h 49m 14s
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
08:02:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.576 km
Perigee altitude
558.685 km
Semi-major axis
6,938.768 km
Eccentricity
0.00028
Inclination
97.5626°
RAAN
282.3106°
Arg. of periapsis
99.7536°
True anomaly
260.36892°
Mean anomaly
260.4006°
Eccentric anomaly
260.38476°
Mean motion
3.75508 °/min
Orbital period
95.87 mins
BSTAR
0.00031839
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 01:31:07.108Z | 156.618° SSE | 2025-09-18 01:34:07.108Z | 73.227° E | 43.064° | 2025-09-18 01:37:07.108Z | 354.913° N |
| 6 mins | 2025-09-18 14:46:07.108Z | 356.472° N | 2025-09-18 14:48:07.108Z | 293.05° NW | 40.886° | 2025-09-18 14:52:07.108Z | 205.353° 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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