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 36597U 26069.52537251 +.00000000 +00000-0 +20415-3 0 00001
2 36597 97.9913 95.7854 0047507 249.7899 109.8213 15.02336578 03
| Epoch (UTC): | 10 March 2026 12:36:32 |
| Eccentricity: | 0.0047507 |
| inclination: | 97.9913° |
| perigee height: | 527 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 95.7854° |
| argument of perigee: | 249.7899° |
| revolutions per day: | 15.02336578 |
| mean anomaly at epoch: | 109.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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