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 55170U 26145.33265329 +.00000000 +00000-0 -21660-4 0 00002
2 55170 87.9151 10.4160 0002091 80.3312 279.8056 13.17649980 07
| Epoch (UTC): | 25 May 2026 07:59:01 |
| Eccentricity: | 0.0002091 |
| inclination: | 87.9151° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4160° |
| argument of perigee: | 80.3312° |
| revolutions per day: | 13.17649980 |
| mean anomaly at epoch: | 279.8056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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