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 50485U 26145.29300553 +.00000000 +00000-0 +15814-3 0 00002
2 50485 87.9173 339.9951 0001527 100.1924 259.9380 13.18685269 05
| Epoch (UTC): | 25 May 2026 07:01:55 |
| Eccentricity: | 0.0001527 |
| inclination: | 87.9173° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9951° |
| argument of perigee: | 100.1924° |
| revolutions per day: | 13.18685269 |
| mean anomaly at epoch: | 259.9380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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