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 56497U 26145.38365000 +.00000000 +00000-0 +47140-4 0 00007
2 56497 69.9990 270.9534 0003611 266.0224 94.0522 14.98331444 01
| Epoch (UTC): | 25 May 2026 09:12:27 |
| Eccentricity: | 0.0003611 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 270.9534° |
| argument of perigee: | 266.0224° |
| revolutions per day: | 14.98331444 |
| mean anomaly at epoch: | 94.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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