BRITE-PL 2, 40119
Orbit data source: Space-Track
BRITE-PL 2, 40119 is a payload satellite owned by CBK (PL) in SSO that was launched on Tue, 19 Aug 2014 UTC via a CHANG ZHENG 4B 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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40119 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
CBKPL/UTIAS
Mission
Operational Civil Astronomy
Bus & Motor
GNB, Unknown motor
Mass
6.8 kg wet, 6.8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.060 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 BRITE-PL 2
1 40119U 14049B 25260.83258956 .00002151 00000-0 21240-3 0 9995
2 40119 97.8952 6.3341 0013241 294.5503 65.4335 14.92982204600781Epoch: 2025-09-17T19:58Z
TLE epoch observation values (Epoch: 2025-09-17T19:58:55.738Z)
Latitude
-0.00004°
Longitude
69.59899°
Altitude
587.856 km
Speed
7.568 km/s
True Right ascension
00h 25m 20s
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
00:10:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.887 km
Perigee altitude
576.445 km
Semi-major axis
6,963.803 km
Eccentricity
0.00132
Inclination
97.8952°
RAAN
6.3341°
Arg. of periapsis
294.5503°
True anomaly
65.57159°
Mean anomaly
65.4335°
Eccentric anomaly
65.50254°
Mean motion
3.73485 °/min
Orbital period
96.39 mins
BSTAR
0.0002124
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Other satellites on launch #49 in the year 2014 (2014-08-19 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.BRITE-PL 2 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 | 2025-09-18 07:21:16.504Z | 178.498° S | 2025-09-18 07:25:16.504Z | 269.704° W | 41.136° | 2025-09-18 07:28:16.504Z | 337.109° NNW |
| 4 mins | 2025-09-18 19:06:16.504Z | 63.278° ENE | 2025-09-18 19:08:16.504Z | 100.283° ESE | 18.75° | 2025-09-18 19:10:16.504Z | 133.566° SE |
| 5 mins | 2025-09-18 20:41:16.504Z | 338.224° N | 2025-09-18 20:43:16.504Z | 295.474° NW | 27.472° | 2025-09-18 20:46:16.504Z | 234.091° WSW |
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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