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 50473U 26145.57902205 +.00000000 +00000-0 -64845-4 0 00002
2 50473 87.9153 10.3603 0001976 87.0265 273.1092 13.17648334 02
| Epoch (UTC): | 25 May 2026 13:53:47 |
| Eccentricity: | 0.0001976 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3603° |
| argument of perigee: | 87.0265° |
| revolutions per day: | 13.17648334 |
| mean anomaly at epoch: | 273.1092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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