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 55994U 26145.55041840 +.00000000 +00000-0 +25048-4 0 00003
2 55994 43.0058 345.5973 0001720 263.1362 96.9294 15.27574534 05
| Epoch (UTC): | 25 May 2026 13:12:36 |
| Eccentricity: | 0.0001720 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.5973° |
| argument of perigee: | 263.1362° |
| revolutions per day: | 15.27574534 |
| mean anomaly at epoch: | 96.9294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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