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 56218U 26145.28470747 +.00000000 +00000-0 +57749-3 0 00007
2 56218 97.2871 63.5946 0006483 109.4721 250.7253 15.89323447 06
| Epoch (UTC): | 25 May 2026 06:49:58 |
| Eccentricity: | 0.0006483 |
| inclination: | 97.2871° |
| perigee height: | 300 km |
| apogee height: | 309 km |
| right ascension of ascending node: | 63.5946° |
| argument of perigee: | 109.4721° |
| revolutions per day: | 15.89323447 |
| mean anomaly at epoch: | 250.7253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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