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 68643U 26144.81173928 +.00000000 +00000-0 +39954-4 0 00000
2 68643 88.9881 323.4019 0010910 67.6999 292.5318 13.67542554 02
| Epoch (UTC): | 24 May 2026 19:28:54 |
| Eccentricity: | 0.0010910 |
| inclination: | 88.9881° |
| perigee height: | 1000 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 323.4019° |
| argument of perigee: | 67.6999° |
| revolutions per day: | 13.67542554 |
| mean anomaly at epoch: | 292.5318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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