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 59928U 26143.76255191 +.00000000 +00000-0 +11358-3 0 00009
2 59928 42.9999 268.6025 0001498 272.9882 87.0798 15.27582476 02
| Epoch (UTC): | 23 May 2026 18:18:04 |
| Eccentricity: | 0.0001498 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 268.6025° |
| argument of perigee: | 272.9882° |
| revolutions per day: | 15.27582476 |
| mean anomaly at epoch: | 87.0798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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