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 55367U 26145.53856080 +.00000000 +00000-0 +23110-4 0 00003
2 55367 42.9997 214.9236 0001258 260.2986 99.7724 15.27571982 09
| Epoch (UTC): | 25 May 2026 12:55:31 |
| Eccentricity: | 0.0001258 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 214.9236° |
| argument of perigee: | 260.2986° |
| revolutions per day: | 15.27571982 |
| mean anomaly at epoch: | 99.7724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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