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 65815U 26145.42136528 +.00000000 +00000-0 +39068-4 0 00007
2 65815 98.6762 86.6344 0001551 94.5908 265.5446 14.19915707 09
| Epoch (UTC): | 25 May 2026 10:06:45 |
| Eccentricity: | 0.0001551 |
| inclination: | 98.6762° |
| perigee height: | 825 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 86.6344° |
| argument of perigee: | 94.5908° |
| revolutions per day: | 14.19915707 |
| mean anomaly at epoch: | 265.5446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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