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 26144.94803058 +.00000000 +00000-0 +00000-0 0 00008
2 36868 8.1640 68.3577 0004233 343.3717 202.1238 1.00277383 07
| Epoch (UTC): | 24 May 2026 22:45:09 |
| Eccentricity: | 0.0004233 |
| inclination: | 8.1640° |
| perigee height: | 35767 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 68.3577° |
| argument of perigee: | 343.3717° |
| revolutions per day: | 1.00277383 |
| mean anomaly at epoch: | 202.1238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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