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 68644U 26144.75935381 +.00000000 +00000-0 +38556-4 0 00000
2 68644 88.9879 323.4132 0011443 74.1908 286.0513 13.67076666 02
| Epoch (UTC): | 24 May 2026 18:13:28 |
| Eccentricity: | 0.0011443 |
| inclination: | 88.9879° |
| perigee height: | 1002 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 323.4132° |
| argument of perigee: | 74.1908° |
| revolutions per day: | 13.67076666 |
| mean anomaly at epoch: | 286.0513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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