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 65982U 26145.54317318 +.00000000 +00000-0 +15236-3 0 00003
2 65982 81.3024 232.9351 0001432 111.5244 248.6065 13.82251692 03
| Epoch (UTC): | 25 May 2026 13:02:10 |
| Eccentricity: | 0.0001432 |
| inclination: | 81.3024° |
| perigee height: | 955 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 232.9351° |
| argument of perigee: | 111.5244° |
| revolutions per day: | 13.82251692 |
| mean anomaly at epoch: | 248.6065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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