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 60562U 26145.46874719 +.00000000 +00000-0 +21470-3 0 00003
2 60562 97.3799 225.7506 0006027 46.0381 314.1357 15.30707080 04
| Epoch (UTC): | 25 May 2026 11:14:59 |
| Eccentricity: | 0.0006027 |
| inclination: | 97.3799° |
| perigee height: | 470 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 225.7506° |
| argument of perigee: | 46.0381° |
| revolutions per day: | 15.30707080 |
| mean anomaly at epoch: | 314.1357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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