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 56720U 26145.32218306 +.00000000 +00000-0 +54856-3 0 00007
2 56720 87.8999 263.7386 0000643 74.8714 285.2487 13.15547108 02
| Epoch (UTC): | 25 May 2026 07:43:56 |
| Eccentricity: | 0.0000643 |
| inclination: | 87.8999° |
| perigee height: | 1201 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 263.7386° |
| argument of perigee: | 74.8714° |
| revolutions per day: | 13.15547108 |
| mean anomaly at epoch: | 285.2487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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