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 39417U 26145.34328483 +.00000000 +00000-0 +33290-3 0 00000
2 39417 97.8107 107.5560 0040371 328.7903 31.0923 15.00990132 07
| Epoch (UTC): | 25 May 2026 08:14:19 |
| Eccentricity: | 0.0040371 |
| inclination: | 97.8107° |
| perigee height: | 536 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 107.5560° |
| argument of perigee: | 328.7903° |
| revolutions per day: | 15.00990132 |
| mean anomaly at epoch: | 31.0923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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