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 56367U 26145.38688660 +.00000000 +00000-0 +00000-0 0 00003
2 56367 0.0643 358.5427 0007504 74.3899 287.1492 5.00115711 06
| Epoch (UTC): | 25 May 2026 09:17:07 |
| Eccentricity: | 0.0007504 |
| inclination: | 0.0643° |
| perigee height: | 8055 km |
| apogee height: | 8077 km |
| right ascension of ascending node: | 358.5427° |
| argument of perigee: | 74.3899° |
| revolutions per day: | 5.00115711 |
| mean anomaly at epoch: | 287.1492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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