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 55167U 26145.59672487 +.00000000 +00000-0 +12630-4 0 00009
2 55167 87.9150 10.3669 0001391 91.4339 268.6951 13.17650195 09
| Epoch (UTC): | 25 May 2026 14:19:17 |
| Eccentricity: | 0.0001391 |
| inclination: | 87.9150° |
| perigee height: | 1193 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3669° |
| argument of perigee: | 91.4339° |
| revolutions per day: | 13.17650195 |
| mean anomaly at epoch: | 268.6951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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