Showing default

NULINK-2, 68994

Orbit data source: Space-Track

NULINK-2, 68994 is a payload satellite owned by NuSpace (SG) in SSO that was launched on Sun, 03 May 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
68994, 2026-100Q
Orbit
SSO
Country
Flag of SGSG / SING
Related business
Manufacturer
NuSpace
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
2026-05-03 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 NULINK-2
1 68994U 26100Q   26317.53678005  .00001375  00000-0  13816-3 0  9996
2 68994  97.7171 212.2460 0001716 120.8021 239.3368 14.92866066 28985
Epoch: 2026-11-13T12:52Z
TLE epoch observation values (Epoch: 2026-11-13T12:52:57.796Z)
Latitude
0.00003°
Longitude
-33.64932°
Altitude
592.659 km
Speed
7.563 km/s
True Right ascension
14h 08m 59s
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
21:09:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.215 km
Perigee altitude
584.825 km
Semi-major axis
6,964.157 km
Eccentricity
0.00017
Inclination
97.7171°
RAAN
212.246°
Arg. of periapsis
120.8021°
True anomaly
239.31989°
Mean anomaly
239.3368°
Eccentric anomaly
239.32834°
Mean motion
3.73457 °/min
Orbital period
96.4 mins
BSTAR
0.00013816
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
|