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 63939U 26145.58335647 +.00000000 +00000-0 +15986-2 0 00003
2 63939 70.0008 80.4755 0003399 260.3500 74.7472 14.98315627 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003399 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.4755° |
| argument of perigee: | 260.3500° |
| revolutions per day: | 14.98315627 |
| mean anomaly at epoch: | 74.7472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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