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 36097U 26145.43220676 +.00000000 +00000-0 +00000-0 0 00006
2 36097 0.0109 304.5609 0002509 129.0733 279.9840 1.00270625 07
| Epoch (UTC): | 25 May 2026 10:22:22 |
| Eccentricity: | 0.0002509 |
| inclination: | 0.0109° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 304.5609° |
| argument of perigee: | 129.0733° |
| revolutions per day: | 1.00270625 |
| mean anomaly at epoch: | 279.9840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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