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: 8 hours ago
TLE from 8 hours ago
0 N1-ATLAS
1 68501U 26067CP 26263.12637178 .00001071 00000-0 11188-3 0 9996
2 68501 97.7740 219.9581 0004926 76.3713 283.8054 14.91752272 25871Epoch: 2026-09-20T03:01Z
TLE epoch observation values (Epoch: 2026-09-20T03:01:58.521Z)
Latitude
-0.00005°
Longitude
175.43924°
Altitude
594.695 km
Speed
7.563 km/s
True Right ascension
14h 39m 49s
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
04:11:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.923 km
Perigee altitude
586.059 km
Semi-major axis
6,967.628 km
Eccentricity
0.00049
Inclination
97.774°
RAAN
219.9581°
Arg. of periapsis
76.3713°
True anomaly
283.75057°
Mean anomaly
283.8054°
Eccentric anomaly
283.77799°
Mean motion
3.73178 °/min
Orbital period
96.47 mins
BSTAR
0.00011188
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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 | 2026-09-20 20:52:22.688Z | 143.581° SSE | 2026-09-20 20:55:22.688Z | 81.216° E | 47.857° | 2026-09-20 20:59:22.688Z | 359.998° N |
| 6 mins | 2026-09-21 10:12:22.688Z | 7.773° NNE | 2026-09-21 10:14:22.688Z | 325.302° NNW | 77.551° | 2026-09-21 10:18:22.688Z | 197.397° SSW |
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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