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 36395U 26145.36038397 +.00000000 +00000-0 +00000-0 0 00006
2 36395 34.6069 86.6854 0001491 38.3240 145.7714 1.00271525 00
| Epoch (UTC): | 25 May 2026 08:38:57 |
| Eccentricity: | 0.0001491 |
| inclination: | 34.6069° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 86.6854° |
| argument of perigee: | 38.3240° |
| revolutions per day: | 1.00271525 |
| mean anomaly at epoch: | 145.7714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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