N1-ATLAS, 68501
Orbit data source: Space-Track
N1-ATLAS, 68501 is an American payload satellite 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.
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68501 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NOVI
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
13 kg wet, 13 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
0.163 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 N1-ATLAS
1 68501U 26067CP 26254.47341503 .00001084 00000-0 11324-3 0 9994
2 68501 97.7723 211.4252 0004938 95.6707 264.5074 14.91728574 24587Epoch: 2026-09-11T11:21Z
TLE epoch observation values (Epoch: 2026-09-11T11:21:43.058Z)
Latitude
-0.00012°
Longitude
50.49954°
Altitude
595.918 km
Speed
7.562 km/s
True Right ascension
14h 05m 42s
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
14:46:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.006 km
Perigee altitude
586.124 km
Semi-major axis
6,967.702 km
Eccentricity
0.00049
Inclination
97.7723°
RAAN
211.4252°
Arg. of periapsis
95.6707°
True anomaly
264.45108°
Mean anomaly
264.5074°
Eccentric anomaly
264.47924°
Mean motion
3.73172 °/min
Orbital period
96.47 mins
BSTAR
0.00011324
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.N1-ATLAS 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-12 10:28:07.338Z | 357.186° N | 2026-09-12 10:31:07.338Z | 288.567° WNW | 50.474° | 2026-09-12 10:35:07.338Z | 211.319° SW |
| 6 mins | 2026-09-12 21:18:07.338Z | 169.881° S | 2026-09-12 21:21:07.338Z | 317.046° NNW | 77.999° | 2026-09-12 21:24:07.338Z | 345.556° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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