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: 22 hours ago
TLE from 22 hours ago
0 BRITE-PL 2
1 40119U 14049B 25323.28562054 .00002383 00000-0 23145-3 0 9994
2 40119 97.8996 69.0364 0015474 86.5096 273.7892 14.93499536610107Epoch: 2025-11-19T06:51Z
TLE epoch observation values (Epoch: 2025-11-19T06:51:17.614Z)
Latitude
-0.00012°
Longitude
-92.34652°
Altitude
589.378 km
Speed
7.566 km/s
True Right ascension
04h 36m 08s
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
01:27:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.83 km
Perigee altitude
573.283 km
Semi-major axis
6,962.194 km
Eccentricity
0.00155
Inclination
97.8996°
RAAN
69.0364°
Arg. of periapsis
86.5096°
True anomaly
273.61225°
Mean anomaly
273.7892°
Eccentric anomaly
273.70073°
Mean motion
3.73615 °/min
Orbital period
96.36 mins
BSTAR
0.00023145
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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 | 2025-11-20 07:05:26.506Z | 160.489° S | 2025-11-20 07:09:26.506Z | 52.791° ENE | 43.904° | 2025-11-20 07:12:26.506Z | 352.183° N |
| 6 mins | 2025-11-20 20:24:26.506Z | 358.395° N | 2025-11-20 20:27:26.506Z | 278.894° WNW | 38.848° | 2025-11-20 20:30:26.506Z | 212.533° SW |
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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