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 55319U 26145.46578763 +.00000000 +00000-0 +23175-3 0 00001
2 55319 69.9992 170.8337 0004005 272.5693 87.5008 14.98314858 00
| Epoch (UTC): | 25 May 2026 11:10:44 |
| Eccentricity: | 0.0004005 |
| inclination: | 69.9992° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.8337° |
| argument of perigee: | 272.5693° |
| revolutions per day: | 14.98314858 |
| mean anomaly at epoch: | 87.5008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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