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 36106U 26145.38673727 +.00000000 +00000-0 +00000-0 0 00000
2 36106 0.0381 102.8269 0002249 317.6103 46.9087 1.00271748 00
| Epoch (UTC): | 25 May 2026 09:16:54 |
| Eccentricity: | 0.0002249 |
| inclination: | 0.0381° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 102.8269° |
| argument of perigee: | 317.6103° |
| revolutions per day: | 1.00271748 |
| mean anomaly at epoch: | 46.9087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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