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.
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68994 intel report (Beta)
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Identifier
Orbit
Country
SG / SINGRelated business
Manufacturer
NuSpace
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 14.5 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 NULINK-2
1 68994U 26100Q 26221.14640108 .00000545 00000-0 58229-4 0 9996
2 68994 97.7263 117.6849 0002362 107.3759 252.7719 14.92695250 14600Epoch: 2026-08-09T03:30Z
TLE epoch observation values (Epoch: 2026-08-09T03:30:49.053Z)
Latitude
0.00001°
Longitude
107.33293°
Altitude
593.068 km
Speed
7.563 km/s
True Right ascension
07h 50m 44s
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
01:53:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.197 km
Perigee altitude
584.907 km
Semi-major axis
6,964.689 km
Eccentricity
0.00024
Inclination
97.7263°
RAAN
117.6849°
Arg. of periapsis
107.3759°
True anomaly
252.74605°
Mean anomaly
252.7719°
Eccentric anomaly
252.75897°
Mean motion
3.73414 °/min
Orbital period
96.41 mins
BSTAR
0.000058229
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.NULINK-2 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 | 2026-08-09 16:31:14.235Z | 128.597° SE | 2026-08-09 16:34:14.235Z | 75.73° E | 26.638° | 2026-08-09 16:37:14.235Z | 15.712° NNE |
| 4 mins | 2026-08-09 18:08:14.235Z | 234.094° WSW | 2026-08-09 18:10:14.235Z | 271.782° WNW | 18.984° | 2026-08-09 18:12:14.235Z | 305.572° NW |
| 6 mins | 2026-08-10 05:50:14.235Z | 25.169° NE | 2026-08-10 05:53:14.235Z | 130.952° SE | 40.193° | 2026-08-10 05:56:14.235Z | 179.939° S |
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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