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 50823U 26145.48233103 +.00000000 +00000-0 +22519-4 0 00006
2 50823 53.2105 184.3858 0001081 77.5830 282.5283 15.08835249 08
| Epoch (UTC): | 25 May 2026 11:34:33 |
| Eccentricity: | 0.0001081 |
| inclination: | 53.2105° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.3858° |
| argument of perigee: | 77.5830° |
| revolutions per day: | 15.08835249 |
| mean anomaly at epoch: | 282.5283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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