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 59081U 26145.31654334 +.00000000 +00000-0 -58567-4 0 00009
2 59081 43.0026 237.6985 0001889 270.9672 89.0963 15.27573165 06
| Epoch (UTC): | 25 May 2026 07:35:49 |
| Eccentricity: | 0.0001889 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.6985° |
| argument of perigee: | 270.9672° |
| revolutions per day: | 15.27573165 |
| mean anomaly at epoch: | 89.0963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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