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 41790U 26145.42154591 +.00000000 +00000-0 +12659-3 0 00009
2 41790 98.1201 208.9522 0053728 322.6261 37.1217 14.79470256 05
| Epoch (UTC): | 25 May 2026 10:07:01 |
| Eccentricity: | 0.0053728 |
| inclination: | 98.1201° |
| perigee height: | 593 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 208.9522° |
| argument of perigee: | 322.6261° |
| revolutions per day: | 14.79470256 |
| mean anomaly at epoch: | 37.1217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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