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 65545U 26145.22856824 +.00000000 +00000-0 +44933-4 0 00000
2 65545 85.9924 54.3944 0001958 96.8573 263.2833 14.12444295 07
| Epoch (UTC): | 25 May 2026 05:29:08 |
| Eccentricity: | 0.0001958 |
| inclination: | 85.9924° |
| perigee height: | 850 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 54.3944° |
| argument of perigee: | 96.8573° |
| revolutions per day: | 14.12444295 |
| mean anomaly at epoch: | 263.2833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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