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 26031.93115272 +.00000000 +00000-0 +28124-3 0 00002
2 05435 50.1395 312.1844 0102460 39.1116 321.7165 14.60038711 05
| Epoch (UTC): | 31 January 2026 22:20:51 |
| Eccentricity: | 0.0102460 |
| inclination: | 50.1395° |
| perigee height: | 621 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 312.1844° |
| argument of perigee: | 39.1116° |
| revolutions per day: | 14.60038711 |
| mean anomaly at epoch: | 321.7165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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