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 65836U 26145.55091859 +.00000000 +00000-0 +56972-3 0 00003
2 65836 53.1585 91.1517 0001386 71.0108 289.1043 15.30210602 03
| Epoch (UTC): | 25 May 2026 13:13:19 |
| Eccentricity: | 0.0001386 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.1517° |
| argument of perigee: | 71.0108° |
| revolutions per day: | 15.30210602 |
| mean anomaly at epoch: | 289.1043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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