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 45060U 26145.49606264 +.00000000 +00000-0 +94267-3 0 00004
2 45060 53.0459 263.3525 0003324 322.1314 37.9462 15.57008078 09
| Epoch (UTC): | 25 May 2026 11:54:19 |
| Eccentricity: | 0.0003324 |
| inclination: | 53.0459° |
| perigee height: | 394 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 263.3525° |
| argument of perigee: | 322.1314° |
| revolutions per day: | 15.57008078 |
| mean anomaly at epoch: | 37.9462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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