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 60524U 26145.49032498 +.00000000 +00000-0 +44751-3 0 00001
2 60524 97.3798 229.6079 0005101 27.2148 332.9365 15.41184799 08
| Epoch (UTC): | 25 May 2026 11:46:04 |
| Eccentricity: | 0.0005101 |
| inclination: | 97.3798° |
| perigee height: | 439 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 229.6079° |
| argument of perigee: | 27.2148° |
| revolutions per day: | 15.41184799 |
| mean anomaly at epoch: | 332.9365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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