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 39418U 26145.57140395 +.00000000 +00000-0 +15821-3 0 00000
2 39418 97.3831 195.6896 0022345 36.6999 323.5757 15.12825030 09
| Epoch (UTC): | 25 May 2026 13:42:49 |
| Eccentricity: | 0.0022345 |
| inclination: | 97.3831° |
| perigee height: | 512 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 195.6896° |
| argument of perigee: | 36.6999° |
| revolutions per day: | 15.12825030 |
| mean anomaly at epoch: | 323.5757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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