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 41240U 26150.52691291 +.00000000 +00000-0 +85185-4 0 00004
2 41240 66.0390 162.9645 0008587 273.3762 86.6274 12.87627629 01
| Epoch (UTC): | 30 May 2026 12:38:45 |
| Eccentricity: | 0.0008587 |
| inclination: | 66.0390° |
| perigee height: | 1304 km |
| apogee height: | 1318 km |
| right ascension of ascending node: | 162.9645° |
| argument of perigee: | 273.3762° |
| revolutions per day: | 12.87627629 |
| mean anomaly at epoch: | 86.6274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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