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 45773U 26145.39654821 +.00000000 +00000-0 +73355-3 0 00001
2 45773 53.1576 192.9865 0004717 345.2446 14.8419 15.36572473 02
| Epoch (UTC): | 25 May 2026 09:31:01 |
| Eccentricity: | 0.0004717 |
| inclination: | 53.1576° |
| perigee height: | 453 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 192.9865° |
| argument of perigee: | 345.2446° |
| revolutions per day: | 15.36572473 |
| mean anomaly at epoch: | 14.8419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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