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 05435U 26133.42489161 +.00000000 +00000-0 +69467-4 0 00006
2 05435 50.1382 220.2561 0101658 50.3548 310.6298 14.60240824 02
| Epoch (UTC): | 13 May 2026 10:11:50 |
| Eccentricity: | 0.0101658 |
| inclination: | 50.1382° |
| perigee height: | 621 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 220.2561° |
| argument of perigee: | 50.3548° |
| revolutions per day: | 14.60240824 |
| mean anomaly at epoch: | 310.6298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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