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 55587U 26145.66493255 +.00000000 +00000-0 +32751-5 0 00004
2 55587 43.0045 290.5416 0001747 266.3854 93.6798 15.27576557 00
| Epoch (UTC): | 25 May 2026 15:57:30 |
| Eccentricity: | 0.0001747 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 290.5416° |
| argument of perigee: | 266.3854° |
| revolutions per day: | 15.27576557 |
| mean anomaly at epoch: | 93.6798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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