Showing default

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.

Loading next visibility...
Identifier
40024, 2014-033Q
Orbit
SSO
Country
Flag of BRBR / BRAZ
Related business
Manufacturer
INPES/UFSM
Mission
Operational Commercial Science
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2014-06-19 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 NANOSAT C BR1
1 40024U 14033Q   26171.34159919  .00014200  00000-0  46858-3 0  9990
2 40024  98.0721 204.0092 0004646 155.2412 204.9051 15.31541409654465
Epoch: 2026-06-20T08:11Z
TLE epoch observation values (Epoch: 2026-06-20T08:11:54.170Z)
Latitude
-0.00001°
Longitude
172.47589°
Altitude
477.186 km
Speed
7.626 km/s
True Right ascension
13h 36m 02s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:43:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.374 km
Perigee altitude
465.012 km
Semi-major axis
6,846.33 km
Eccentricity
0.00046
Inclination
98.0721°
RAAN
204.0092°
Arg. of periapsis
155.2412°
True anomaly
204.88269°
Mean anomaly
204.9051°
Eccentric anomaly
204.89389°
Mean motion
3.83139 °/min
Orbital period
93.96 mins
BSTAR
0.00046858
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|