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 26113.48378351 +.00000000 +00000-0 +00000-0 0 00003
2 36108 0.3872 85.3500 0000178 164.1089 6.2533 1.00268276 07
| Epoch (UTC): | 23 April 2026 11:36:38 |
| Eccentricity: | 0.0000178 |
| inclination: | 0.3872° |
| perigee height: | 35787 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 85.3500° |
| argument of perigee: | 164.1089° |
| revolutions per day: | 1.00268276 |
| mean anomaly at epoch: | 6.2533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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