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 36416U 26131.78339766 +.00000000 +00000-0 +15786-3 0 00005
2 36416 63.3832 142.7301 0696313 3.0948 357.4072 13.73085267 07
| Epoch (UTC): | 11 May 2026 18:48:05 |
| Eccentricity: | 0.0696313 |
| inclination: | 63.3832° |
| perigee height: | 476 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 142.7301° |
| argument of perigee: | 3.0948° |
| revolutions per day: | 13.73085267 |
| mean anomaly at epoch: | 357.4072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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