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 59398U 26145.60724477 +.00000000 +00000-0 +32849-4 0 00002
2 59398 43.0043 341.4152 0001464 267.7183 92.3501 15.27573158 03
| Epoch (UTC): | 25 May 2026 14:34:25 |
| Eccentricity: | 0.0001464 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.4152° |
| argument of perigee: | 267.7183° |
| revolutions per day: | 15.27573158 |
| mean anomaly at epoch: | 92.3501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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