NULINK-1, 69002
Orbit data source: Space-Track
NULINK-1, 69002 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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69002 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-1
1 69002U 26100Y 26168.65201523 .00002813 00000-0 27815-3 0 9993
2 69002 97.7351 66.1549 0002213 34.2762 325.8599 14.92692476 6764Epoch: 2026-06-17T15:38Z
TLE epoch observation values (Epoch: 2026-06-17T15:38:54.115Z)
Latitude
-0.00013°
Longitude
-74.47719°
Altitude
591.312 km
Speed
7.565 km/s
True Right ascension
04h 24m 37s
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
12:14:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.102 km
Perigee altitude
585.02 km
Semi-major axis
6,964.698 km
Eccentricity
0.00022
Inclination
97.7351°
RAAN
66.1549°
Arg. of periapsis
34.2762°
True anomaly
325.84566°
Mean anomaly
325.8599°
Eccentric anomaly
325.85278°
Mean motion
3.73413 °/min
Orbital period
96.41 mins
BSTAR
0.00027815
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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-1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-18 05:06:50.583Z | 57.525° ENE | 2026-06-18 05:08:50.583Z | 91.108° ESE | 17.811° | 2026-06-18 05:11:50.583Z | 138.501° SSE |
| 5 mins | 2026-06-18 06:42:50.583Z | 331.808° NNW | 2026-06-18 06:44:50.583Z | 279.723° WNW | 28.14° | 2026-06-18 06:47:50.583Z | 228.022° WSW |
| 6 mins | 2026-06-18 17:31:50.583Z | 193.276° SSW | 2026-06-18 17:33:50.583Z | 252.42° W | 38.661° | 2026-06-18 17:37:50.583Z | 337.334° 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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