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 50212U 26145.59204846 +.00000000 +00000-0 +00000-0 0 00009
2 50212 0.0683 341.8091 0004181 12.4315 144.0597 1.00272417 09
| Epoch (UTC): | 25 May 2026 14:12:32 |
| Eccentricity: | 0.0004181 |
| inclination: | 0.0683° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 341.8091° |
| argument of perigee: | 12.4315° |
| revolutions per day: | 1.00272417 |
| mean anomaly at epoch: | 144.0597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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