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 39484U 26145.55418178 +.00000000 +00000-0 -10295-2 0 00008
2 39484 82.4883 184.1677 0022269 142.3797 217.8846 12.42878800 07
| Epoch (UTC): | 25 May 2026 13:18:01 |
| Eccentricity: | 0.0022269 |
| inclination: | 82.4883° |
| perigee height: | 1477 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 184.1677° |
| argument of perigee: | 142.3797° |
| revolutions per day: | 12.42878800 |
| mean anomaly at epoch: | 217.8846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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