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 56122U 26145.55236992 +.00000000 +00000-0 +23507-4 0 00009
2 56122 43.0060 84.3139 0001558 285.2837 74.7843 15.27577536 04
| Epoch (UTC): | 25 May 2026 13:15:24 |
| Eccentricity: | 0.0001558 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.3139° |
| argument of perigee: | 285.2837° |
| revolutions per day: | 15.27577536 |
| mean anomaly at epoch: | 74.7843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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