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: 1 day ago
TLE from 1 day ago
0 N1-ATLAS
1 68501U 26067CP 26259.30299140 .00001720 00000-0 17635-3 0 9998
2 68501 97.7733 216.1876 0004917 84.7998 275.3782 14.91743841 25301Epoch: 2026-09-16T07:16Z
TLE epoch observation values (Epoch: 2026-09-16T07:16:18.456Z)
Latitude
-0.00003°
Longitude
111.85418°
Altitude
595.22 km
Speed
7.562 km/s
True Right ascension
14h 24m 45s
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
06:19:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.943 km
Perigee altitude
586.091 km
Semi-major axis
6,967.654 km
Eccentricity
0.00049
Inclination
97.7733°
RAAN
216.1876°
Arg. of periapsis
84.7998°
True anomaly
275.3221°
Mean anomaly
275.3782°
Eccentric anomaly
275.35015°
Mean motion
3.73176 °/min
Orbital period
96.47 mins
BSTAR
0.00017635
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-17 20:26:20.395Z | 121.016° SE | 2026-09-17 20:29:20.395Z | 70.363° E | 24.817° | 2026-09-17 20:32:20.395Z | 18.186° NNE |
| 5 mins | 2026-09-17 22:03:20.395Z | 231.35° WSW | 2026-09-17 22:05:20.395Z | 275.818° WNW | 24.722° | 2026-09-17 22:08:20.395Z | 321.059° NNW |
| 6 mins | 2026-09-18 09:45:20.395Z | 29.624° NE | 2026-09-18 09:48:20.395Z | 103.113° ESE | 48.557° | 2026-09-18 09:51:20.395Z | 170.311° S |
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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