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 56299U 26145.22675059 +.00000000 +00000-0 -72948-4 0 00003
2 56299 43.0008 125.4664 0000776 291.6153 68.4616 15.27585586 06
| Epoch (UTC): | 25 May 2026 05:26:31 |
| Eccentricity: | 0.0000776 |
| inclination: | 43.0008° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.4664° |
| argument of perigee: | 291.6153° |
| revolutions per day: | 15.27585586 |
| mean anomaly at epoch: | 68.4616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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