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 50202U 26145.56054216 +.00000000 +00000-0 +24417-3 0 00000
2 50202 53.2135 254.0338 0001068 99.4481 260.6632 15.08832766 06
| Epoch (UTC): | 25 May 2026 13:27:10 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 254.0338° |
| argument of perigee: | 99.4481° |
| revolutions per day: | 15.08832766 |
| mean anomaly at epoch: | 260.6632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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