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 59198U 26145.03615507 +.00000000 +00000-0 -50105-4 0 00006
2 59198 43.0030 21.7120 0000312 216.7422 143.3409 15.27582295 07
| Epoch (UTC): | 25 May 2026 00:52:03 |
| Eccentricity: | 0.0000312 |
| inclination: | 43.0030° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 21.7120° |
| argument of perigee: | 216.7422° |
| revolutions per day: | 15.27582295 |
| mean anomaly at epoch: | 143.3409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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