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 55317U 26145.47413323 +.00000000 +00000-0 -37638-5 0 00002
2 55317 69.9988 170.8893 0003859 267.2238 92.8480 14.98330063 01
| Epoch (UTC): | 25 May 2026 11:22:45 |
| Eccentricity: | 0.0003859 |
| inclination: | 69.9988° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.8893° |
| argument of perigee: | 267.2238° |
| revolutions per day: | 14.98330063 |
| mean anomaly at epoch: | 92.8480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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