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 59868U 26145.33713940 +.00000000 +00000-0 -19236-4 0 00003
2 59868 43.0009 164.7758 0001036 271.5557 88.5176 15.27577060 09
| Epoch (UTC): | 25 May 2026 08:05:28 |
| Eccentricity: | 0.0001036 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.7758° |
| argument of perigee: | 271.5557° |
| revolutions per day: | 15.27577060 |
| mean anomaly at epoch: | 88.5176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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