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 35491U 26145.54280769 +.00000000 +00000-0 +00000-0 0 00004
2 35491 1.6342 83.2992 0001903 345.9542 163.9193 1.00117172 00
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0001903 |
| inclination: | 1.6342° |
| perigee height: | 35822 km |
| apogee height: | 35838 km |
| right ascension of ascending node: | 83.2992° |
| argument of perigee: | 345.9542° |
| revolutions per day: | 1.00117172 |
| mean anomaly at epoch: | 163.9193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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