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 55341U 26145.54447854 +.00000000 +00000-0 +19828-4 0 00002
2 55341 43.0042 229.6946 0001647 277.3913 82.6752 15.27575564 08
| Epoch (UTC): | 25 May 2026 13:04:02 |
| Eccentricity: | 0.0001647 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.6946° |
| argument of perigee: | 277.3913° |
| revolutions per day: | 15.27575564 |
| mean anomaly at epoch: | 82.6752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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