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 36108U 26140.56732185 +.00000000 +00000-0 +00000-0 0 00001
2 36108 0.3617 85.5973 0000289 220.8779 6.0053 1.00271176 07
| Epoch (UTC): | 20 May 2026 13:36:56 |
| Eccentricity: | 0.0000289 |
| inclination: | 0.3617° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 85.5973° |
| argument of perigee: | 220.8779° |
| revolutions per day: | 1.00271176 |
| mean anomaly at epoch: | 6.0053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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