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 55477U 26145.55877863 +.00000000 +00000-0 +10140-3 0 00007
2 55477 43.0001 247.1032 0001658 274.3886 85.6776 15.27573783 02
| Epoch (UTC): | 25 May 2026 13:24:38 |
| Eccentricity: | 0.0001658 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.1032° |
| argument of perigee: | 274.3886° |
| revolutions per day: | 15.27573783 |
| mean anomaly at epoch: | 85.6776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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