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: 4 hours ago
TLE from 4 hours ago
0 TIANPING 3A-01
1 61614U 24189A 25298.32360678 .00005708 00000-0 45194-3 0 9999
2 61614 97.5545 320.5736 0002199 76.5890 283.5580 15.00968142 55251Epoch: 2025-10-25T07:45Z
TLE epoch observation values (Epoch: 2025-10-25T07:45:59.625Z)
Latitude
0.00002°
Longitude
170.11936°
Altitude
566.612 km
Speed
7.578 km/s
True Right ascension
21h 22m 17s
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
07:24:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.433 km
Perigee altitude
559.381 km
Semi-major axis
6,939.044 km
Eccentricity
0.00022
Inclination
97.5545°
RAAN
320.5736°
Arg. of periapsis
76.589°
True anomaly
283.5335°
Mean anomaly
283.558°
Eccentric anomaly
283.54575°
Mean motion
3.75486 °/min
Orbital period
95.88 mins
BSTAR
0.00045194
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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 | 2025-10-25 14:43:27.185Z | 3.069° NNE | 2025-10-25 14:47:27.185Z | 253.407° W | 39.184° | 2025-10-25 14:50:27.185Z | 207.272° SW |
| 6 mins | 2025-10-26 01:30:27.185Z | 155.164° SSE | 2025-10-26 01:32:27.185Z | 114.147° SE | 42.332° | 2025-10-26 01:36:27.185Z | 353.147° 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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