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 55998U 26145.59652282 +.00000000 +00000-0 +23649-4 0 00004
2 55998 43.0042 345.0795 0001364 267.8608 92.2088 15.27578262 09
| Epoch (UTC): | 25 May 2026 14:18:59 |
| Eccentricity: | 0.0001364 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.0795° |
| argument of perigee: | 267.8608° |
| revolutions per day: | 15.27578262 |
| mean anomaly at epoch: | 92.2088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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