NANOSAT C BR1, 40024
Orbit data source: Space-Track
NANOSAT C BR1, 40024 is a Brazilian payload satellite in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40024 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / BRAZRelated business
Manufacturer
INPES/UFSM
Mission
Operational Commercial Science
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 NANOSAT C BR1
1 40024U 14033Q 25338.58600823 .00033986 00000-0 13915-2 0 9994
2 40024 98.0897 349.5994 0005301 124.9633 235.2101 15.24220628624269Epoch: 2025-12-04T14:03Z
TLE epoch observation values (Epoch: 2025-12-04T14:03:51.111Z)
Latitude
0.00002°
Longitude
64.99611°
Altitude
498.282 km
Speed
7.614 km/s
True Right ascension
23h 18m 23s
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
07:27:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.758 km
Perigee altitude
486.477 km
Semi-major axis
6,868.255 km
Eccentricity
0.00053
Inclination
98.0897°
RAAN
349.5994°
Arg. of periapsis
124.9633°
True anomaly
235.16023°
Mean anomaly
235.2101°
Eccentric anomaly
235.18516°
Mean motion
3.81306 °/min
Orbital period
94.41 mins
BSTAR
0.0013915
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.NANOSAT C BR1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-05 14:16:34.059Z | 337.644° N | 2025-12-05 14:18:34.059Z | 266.866° W | 30.676° | 2025-12-05 14:20:34.059Z | 224.761° SW |
| 6 mins | 2025-12-06 00:51:34.059Z | 162.001° S | 2025-12-06 00:54:34.059Z | 8.305° NNE | 42.663° | 2025-12-06 00:57:34.059Z | 349.456° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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