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 36868U 26140.45642700 +.00000000 +00000-0 +00000-0 0 00005
2 36868 8.1525 68.4114 0004018 339.6810 24.2896 1.00274625 09
| Epoch (UTC): | 20 May 2026 10:57:15 |
| Eccentricity: | 0.0004018 |
| inclination: | 8.1525° |
| perigee height: | 35769 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 68.4114° |
| argument of perigee: | 339.6810° |
| revolutions per day: | 1.00274625 |
| mean anomaly at epoch: | 24.2896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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