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 56055U 26145.53482939 +.00000000 +00000-0 +14842-3 0 00007
2 56055 87.9106 233.2718 0002360 105.9354 254.2037 13.16592962 05
| Epoch (UTC): | 25 May 2026 12:50:09 |
| Eccentricity: | 0.0002360 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2718° |
| argument of perigee: | 105.9354° |
| revolutions per day: | 13.16592962 |
| mean anomaly at epoch: | 254.2037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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