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 56715U 26145.52057752 +.00000000 +00000-0 +18550-3 0 00000
2 56715 87.9109 233.2696 0002562 105.8111 254.3302 13.16592951 04
| Epoch (UTC): | 25 May 2026 12:29:37 |
| Eccentricity: | 0.0002562 |
| inclination: | 87.9109° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2696° |
| argument of perigee: | 105.8111° |
| revolutions per day: | 13.16592951 |
| mean anomaly at epoch: | 254.3302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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