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 55805U 26145.43377086 +.00000000 +00000-0 +62003-4 0 00007
2 55805 87.9156 309.4999 0001623 92.4757 267.6562 13.19726532 03
| Epoch (UTC): | 25 May 2026 10:24:37 |
| Eccentricity: | 0.0001623 |
| inclination: | 87.9156° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4999° |
| argument of perigee: | 92.4757° |
| revolutions per day: | 13.19726532 |
| mean anomaly at epoch: | 267.6562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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