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 56521U 26145.42964659 +.00000000 +00000-0 +11891-4 0 00009
2 56521 43.0018 142.6968 0000943 274.2685 85.8059 15.27577684 00
| Epoch (UTC): | 25 May 2026 10:18:41 |
| Eccentricity: | 0.0000943 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.6968° |
| argument of perigee: | 274.2685° |
| revolutions per day: | 15.27577684 |
| mean anomaly at epoch: | 85.8059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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