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 55011U 26145.62198889 +.00000000 +00000-0 +55469-3 0 00006
2 55011 97.3231 210.5042 0006235 187.4099 172.7060 15.47504307 06
| Epoch (UTC): | 25 May 2026 14:55:39 |
| Eccentricity: | 0.0006235 |
| inclination: | 97.3231° |
| perigee height: | 420 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 210.5042° |
| argument of perigee: | 187.4099° |
| revolutions per day: | 15.47504307 |
| mean anomaly at epoch: | 172.7060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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