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 26053.69583865 +.00000000 +00000-0 +22823-3 0 00006
2 05435 50.1375 215.2811 0102353 118.7909 242.3346 14.60096906 04
| Epoch (UTC): | 22 February 2026 16:42:00 |
| Eccentricity: | 0.0102353 |
| inclination: | 50.1375° |
| perigee height: | 620 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 215.2811° |
| argument of perigee: | 118.7909° |
| revolutions per day: | 14.60096906 |
| mean anomaly at epoch: | 242.3346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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