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 spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 NULINK-2
1 68994U 26100Q 26168.65625333 .00002863 00000-0 28392-3 0 9997
2 68994 97.7331 66.1414 0001282 47.5654 312.5674 14.92562873 6779Epoch: 2026-06-17T15:45Z
TLE epoch observation values (Epoch: 2026-06-17T15:45:00.287Z)
Latitude
0.00001°
Longitude
-76.0206°
Altitude
592.387 km
Speed
7.564 km/s
True Right ascension
04h 24m 33s
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
12:54:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.857 km
Perigee altitude
586.071 km
Semi-major axis
6,965.101 km
Eccentricity
0.00013
Inclination
97.7331°
RAAN
66.1414°
Arg. of periapsis
47.5654°
True anomaly
312.55658°
Mean anomaly
312.5674°
Eccentric anomaly
312.56199°
Mean motion
3.73381 °/min
Orbital period
96.42 mins
BSTAR
0.00028392
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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 | 2026-06-18 05:12:01.853Z | 44.41° NE | 2026-06-18 05:15:01.853Z | 92.546° ESE | 20.446° | 2026-06-18 05:18:01.853Z | 143.073° SSE |
| 5 mins | 2026-06-18 06:49:01.853Z | 326.754° NNW | 2026-06-18 06:51:01.853Z | 279.172° WNW | 24.855° | 2026-06-18 06:54:01.853Z | 231.944° WSW |
| 6 mins | 2026-06-18 17:38:01.853Z | 201.02° SSW | 2026-06-18 17:40:01.853Z | 255.362° W | 35.047° | 2026-06-18 17:44:01.853Z | 334.051° NNW |
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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