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 55588U 26145.66751940 +.00000000 +00000-0 +15553-4 0 00003
2 55588 43.0056 290.6403 0002122 278.2796 81.7815 15.27576227 07
| Epoch (UTC): | 25 May 2026 16:01:13 |
| Eccentricity: | 0.0002122 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 290.6403° |
| argument of perigee: | 278.2796° |
| revolutions per day: | 15.27576227 |
| mean anomaly at epoch: | 81.7815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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