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 68641U 26144.78239200 +.00000000 +00000-0 +40212-4 0 00009
2 68641 88.9876 323.4155 0010627 75.2262 285.0073 13.62969308 08
| Epoch (UTC): | 24 May 2026 18:46:38 |
| Eccentricity: | 0.0010627 |
| inclination: | 88.9876° |
| perigee height: | 1017 km |
| apogee height: | 1033 km |
| right ascension of ascending node: | 323.4155° |
| argument of perigee: | 75.2262° |
| revolutions per day: | 13.62969308 |
| mean anomaly at epoch: | 285.0073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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