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 50169U 26145.58537049 +.00000000 +00000-0 +10134-4 0 00006
2 50169 53.2133 263.9182 0001004 87.4952 272.6155 15.08834922 01
| Epoch (UTC): | 25 May 2026 14:02:56 |
| Eccentricity: | 0.0001004 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 263.9182° |
| argument of perigee: | 87.4952° |
| revolutions per day: | 15.08834922 |
| mean anomaly at epoch: | 272.6155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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