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 68652U 26145.29912984 +.00000000 +00000-0 +43838-4 0 00002
2 68652 88.9874 323.3456 0010386 64.4212 295.8019 13.63414908 09
| Epoch (UTC): | 25 May 2026 07:10:44 |
| Eccentricity: | 0.0010386 |
| inclination: | 88.9874° |
| perigee height: | 1016 km |
| apogee height: | 1031 km |
| right ascension of ascending node: | 323.3456° |
| argument of perigee: | 64.4212° |
| revolutions per day: | 13.63414908 |
| mean anomaly at epoch: | 295.8019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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