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 39765U 26053.79199774 +.00000000 +00000-0 -24058-4 0 00006
2 39765 82.4541 329.6335 0230455 270.2848 87.1851 12.82900617 03
| Epoch (UTC): | 22 February 2026 19:00:28 |
| Eccentricity: | 0.0230455 |
| inclination: | 82.4541° |
| perigee height: | 1152 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 329.6335° |
| argument of perigee: | 270.2848° |
| revolutions per day: | 12.82900617 |
| mean anomaly at epoch: | 87.1851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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