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 55575U 26145.52982609 +.00000000 +00000-0 +20612-4 0 00004
2 55575 43.0013 294.7349 0001169 275.3416 84.7302 15.27571611 03
| Epoch (UTC): | 25 May 2026 12:42:56 |
| Eccentricity: | 0.0001169 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 294.7349° |
| argument of perigee: | 275.3416° |
| revolutions per day: | 15.27571611 |
| mean anomaly at epoch: | 84.7302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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