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 55822U 26145.66555448 +.00000000 +00000-0 -55109-3 0 00000
2 55822 87.8933 294.2427 0001741 86.7892 273.3437 13.14501094 02
| Epoch (UTC): | 25 May 2026 15:58:23 |
| Eccentricity: | 0.0001741 |
| inclination: | 87.8933° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2427° |
| argument of perigee: | 86.7892° |
| revolutions per day: | 13.14501094 |
| mean anomaly at epoch: | 273.3437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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