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 45197U 26145.43695477 +.00000000 +00000-0 +12442-2 0 00007
2 45197 53.1582 42.4902 0003005 84.8649 275.2696 15.33638361 06
| Epoch (UTC): | 25 May 2026 10:29:12 |
| Eccentricity: | 0.0003005 |
| inclination: | 53.1582° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 42.4902° |
| argument of perigee: | 84.8649° |
| revolutions per day: | 15.33638361 |
| mean anomaly at epoch: | 275.2696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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