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 55810U 26145.46379001 +.00000000 +00000-0 +25670-3 0 00003
2 55810 87.9150 309.5059 0001506 92.9390 267.1915 13.19726309 08
| Epoch (UTC): | 25 May 2026 11:07:51 |
| Eccentricity: | 0.0001506 |
| inclination: | 87.9150° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5059° |
| argument of perigee: | 92.9390° |
| revolutions per day: | 13.19726309 |
| mean anomaly at epoch: | 267.1915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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