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 19650U 26105.35245226 +.00000000 +00000-0 -32000-4 0 00007
2 19650 70.9989 74.3509 0016041 308.9490 51.0203 14.16159994 08
| Epoch (UTC): | 15 April 2026 08:27:31 |
| Eccentricity: | 0.0016041 |
| inclination: | 70.9989° |
| perigee height: | 827 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 74.3509° |
| argument of perigee: | 308.9490° |
| revolutions per day: | 14.16159994 |
| mean anomaly at epoch: | 51.0203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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