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 39360U 26145.56067499 +.00000000 +00000-0 +00000-0 0 00008
2 39360 0.0041 353.6076 0001747 141.8756 193.1440 1.00272326 04
| Epoch (UTC): | 25 May 2026 13:27:22 |
| Eccentricity: | 0.0001747 |
| inclination: | 0.0041° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 353.6076° |
| argument of perigee: | 141.8756° |
| revolutions per day: | 1.00272326 |
| mean anomaly at epoch: | 193.1440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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