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 39771U 26105.56305193 +.00000000 +00000-0 +16220-3 0 00000
2 39771 98.1976 96.9788 0008979 12.2581 347.8865 15.14000952 06
| Epoch (UTC): | 15 April 2026 13:30:47 |
| Eccentricity: | 0.0008979 |
| inclination: | 98.1976° |
| perigee height: | 518 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 96.9788° |
| argument of perigee: | 12.2581° |
| revolutions per day: | 15.14000952 |
| mean anomaly at epoch: | 347.8865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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