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 59095U 26145.53069421 +.00000000 +00000-0 +75868-4 0 00007
2 59095 42.9990 236.7169 0001246 261.4813 98.5898 15.27580210 03
| Epoch (UTC): | 25 May 2026 12:44:11 |
| Eccentricity: | 0.0001246 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.7169° |
| argument of perigee: | 261.4813° |
| revolutions per day: | 15.27580210 |
| mean anomaly at epoch: | 98.5898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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