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: 9 hours ago
TLE from 9 hours ago
0 NANOSAT C BR1
1 40024U 14033Q 25287.86872185 .00016641 00000-0 73075-3 0 9993
2 40024 98.0948 294.9690 0003145 350.3230 9.7943 15.22017168616545Epoch: 2025-10-14T20:50Z
TLE epoch observation values (Epoch: 2025-10-14T20:50:57.567Z)
Latitude
-0.00005°
Longitude
-41.42182°
Altitude
500.697 km
Speed
7.615 km/s
True Right ascension
19h 39m 52s
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
00:09:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.913 km
Perigee altitude
494.589 km
Semi-major axis
6,874.888 km
Eccentricity
0.00031
Inclination
98.0948°
RAAN
294.969°
Arg. of periapsis
350.323°
True anomaly
9.80043°
Mean anomaly
9.7943°
Eccentric anomaly
9.79737°
Mean motion
3.80754 °/min
Orbital period
94.55 mins
BSTAR
0.00073075
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-15 13:11:57.316Z | 29.591° NE | 2025-10-15 13:14:57.316Z | 125.078° SE | 35.774° | 2025-10-15 13:17:57.316Z | 176.05° S |
| 4 mins | 2025-10-15 23:49:57.316Z | 105.377° ESE | 2025-10-15 23:51:57.316Z | 60.876° ENE | 20.127° | 2025-10-15 23:53:57.316Z | 23.324° NE |
| 4 mins | 2025-10-16 01:23:57.316Z | 235.198° WSW | 2025-10-16 01:24:57.316Z | 257.769° W | 20.108° | 2025-10-16 01:27:57.316Z | 314.806° NW |
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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