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 50573U 26145.64154909 +.00000000 +00000-0 +11371-3 0 00005
2 50573 88.9702 325.9201 0009047 144.8812 215.3046 15.46147069 00
| Epoch (UTC): | 25 May 2026 15:23:49 |
| Eccentricity: | 0.0009047 |
| inclination: | 88.9702° |
| perigee height: | 422 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 325.9201° |
| argument of perigee: | 144.8812° |
| revolutions per day: | 15.46147069 |
| mean anomaly at epoch: | 215.3046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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