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 36397U 26145.12683769 +.00000000 +00000-0 +00000-0 0 00001
2 36397 0.0145 298.4165 0002722 160.1693 113.5979 1.00270593 06
| Epoch (UTC): | 25 May 2026 03:02:38 |
| Eccentricity: | 0.0002722 |
| inclination: | 0.0145° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 298.4165° |
| argument of perigee: | 160.1693° |
| revolutions per day: | 1.00270593 |
| mean anomaly at epoch: | 113.5979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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