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 39362U 26066.82524538 +.00000000 +00000-0 +89402-3 0 00009
2 39362 49.5701 11.4249 5125182 128.5912 289.6632 5.38841855 07
| Epoch (UTC): | 07 March 2026 19:48:21 |
| Eccentricity: | 0.5125182 |
| inclination: | 49.5701° |
| perigee height: | 322 km |
| apogee height: | 14409 km |
| right ascension of ascending node: | 11.4249° |
| argument of perigee: | 128.5912° |
| revolutions per day: | 5.38841855 |
| mean anomaly at epoch: | 289.6632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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