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 45794U 26145.56223331 +.00000000 +00000-0 +40131-3 0 00007
2 45794 97.5354 279.0459 0012332 156.8771 203.3028 15.31993301 09
| Epoch (UTC): | 25 May 2026 13:29:36 |
| Eccentricity: | 0.0012332 |
| inclination: | 97.5354° |
| perigee height: | 461 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 279.0459° |
| argument of perigee: | 156.8771° |
| revolutions per day: | 15.31993301 |
| mean anomaly at epoch: | 203.3028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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