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 56016U 26145.59588669 +.00000000 +00000-0 -18220-3 0 00002
2 56016 43.0019 331.2072 0000973 260.2721 99.8020 15.27596661 00
| Epoch (UTC): | 25 May 2026 14:18:04 |
| Eccentricity: | 0.0000973 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.2072° |
| argument of perigee: | 260.2721° |
| revolutions per day: | 15.27596661 |
| mean anomaly at epoch: | 99.8020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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