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 56069U 26145.50317137 +.00000000 +00000-0 -72766-4 0 00007
2 56069 87.9107 233.2876 0002534 92.3424 267.7998 13.16595159 02
| Epoch (UTC): | 25 May 2026 12:04:34 |
| Eccentricity: | 0.0002534 |
| inclination: | 87.9107° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2876° |
| argument of perigee: | 92.3424° |
| revolutions per day: | 13.16595159 |
| mean anomaly at epoch: | 267.7998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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