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 68636U 26144.73566323 +.00000000 +00000-0 +39978-4 0 00004
2 68636 88.9878 323.4276 0011681 66.5483 293.6903 13.65209094 06
| Epoch (UTC): | 24 May 2026 17:39:21 |
| Eccentricity: | 0.0011681 |
| inclination: | 88.9878° |
| perigee height: | 1008 km |
| apogee height: | 1025 km |
| right ascension of ascending node: | 323.4276° |
| argument of perigee: | 66.5483° |
| revolutions per day: | 13.65209094 |
| mean anomaly at epoch: | 293.6903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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