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 55950U 26145.21428328 +.00000000 +00000-0 +48950-4 0 00005
2 55950 70.0002 71.6002 0002944 269.6917 90.3905 14.98330981 02
| Epoch (UTC): | 25 May 2026 05:08:34 |
| Eccentricity: | 0.0002944 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 71.6002° |
| argument of perigee: | 269.6917° |
| revolutions per day: | 14.98330981 |
| mean anomaly at epoch: | 90.3905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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