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 55168U 26145.58491479 +.00000000 +00000-0 -84347-4 0 00004
2 55168 87.9153 10.3696 0002285 90.9059 269.2334 13.17650623 07
| Epoch (UTC): | 25 May 2026 14:02:16 |
| Eccentricity: | 0.0002285 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3696° |
| argument of perigee: | 90.9059° |
| revolutions per day: | 13.17650623 |
| mean anomaly at epoch: | 269.2334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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