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 60525U 26145.50898866 +.00000000 +00000-0 +40978-3 0 00000
2 60525 97.3719 231.1780 0005015 17.0279 343.1136 15.44111998 09
| Epoch (UTC): | 25 May 2026 12:12:56 |
| Eccentricity: | 0.0005015 |
| inclination: | 97.3719° |
| perigee height: | 431 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 231.1780° |
| argument of perigee: | 17.0279° |
| revolutions per day: | 15.44111998 |
| mean anomaly at epoch: | 343.1136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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