View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 41794U 26144.97075005 +.00000000 +00000-0 +00000-0 0 00008
2 41794 0.0146 295.5559 0001678 120.4751 320.8047 1.00272870 01
| Epoch (UTC): | 24 May 2026 23:17:52 |
| Eccentricity: | 0.0001678 |
| inclination: | 0.0146° |
| perigee height: | 35779 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 295.5559° |
| argument of perigee: | 120.4751° |
| revolutions per day: | 1.00272870 |
| mean anomaly at epoch: | 320.8047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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