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 36599U 26106.82330338 +.00000000 +00000-0 +55490-4 0 00007
2 36599 98.0234 308.4946 0053625 39.5642 320.9453 14.59091672 04
| Epoch (UTC): | 16 April 2026 19:45:33 |
| Eccentricity: | 0.0053625 |
| inclination: | 98.0234° |
| perigee height: | 658 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 308.4946° |
| argument of perigee: | 39.5642° |
| revolutions per day: | 14.59091672 |
| mean anomaly at epoch: | 320.9453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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