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 50818U 26145.46760469 +.00000000 +00000-0 -28844-3 0 00005
2 50818 53.2104 184.4517 0000933 82.3641 277.7457 15.08858865 01
| Epoch (UTC): | 25 May 2026 11:13:21 |
| Eccentricity: | 0.0000933 |
| inclination: | 53.2104° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 184.4517° |
| argument of perigee: | 82.3641° |
| revolutions per day: | 15.08858865 |
| mean anomaly at epoch: | 277.7457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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