Showing default

NUSAT-53 (JANE GOODALL), 68432

Orbit data source: Space-Track

NUSAT-53 (JANE GOODALL), 68432 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
68432, 2026-067S
Orbit
SSO
Country
Flag of ARAR / ARGN
Related business
Manufacturer
URUGUS S.A.
Mission
Operational Commercial Imaging
Bus & Motor
NEWSAT V, Unknown motor
Mass
41.5 kg wet, 38.5 kg dry
Launch date (UTC)
2026-03-30 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 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 NUSAT-53 (JANE GOODALL)
1 68432U 26067S   26258.84636497  .00004966  00000-0  23852-3 0  9992
2 68432  97.4661 216.1916 0004545  73.8429 286.3305 15.19288821 25701
Epoch: 2026-09-15T20:18Z
TLE epoch observation values (Epoch: 2026-09-15T20:18:45.933Z)
Latitude
-0.00007°
Longitude
-83.30623°
Altitude
510.197 km
Speed
7.609 km/s
True Right ascension
14h 24m 45s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
02:59:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.086 km
Perigee altitude
501.83 km
Semi-major axis
6,883.095 km
Eccentricity
0.00045
Inclination
97.4661°
RAAN
216.1916°
Arg. of periapsis
73.8429°
True anomaly
286.28051°
Mean anomaly
286.3305°
Eccentric anomaly
286.30551°
Mean motion
3.80073 °/min
Orbital period
94.72 mins
BSTAR
0.00023852
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
|