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 59267U 26145.54077477 +.00000000 +00000-0 +13549-4 0 00007
2 59267 53.1594 184.1114 0001077 91.0193 269.0931 15.30192116 05
| Epoch (UTC): | 25 May 2026 12:58:42 |
| Eccentricity: | 0.0001077 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.1114° |
| argument of perigee: | 91.0193° |
| revolutions per day: | 15.30192116 |
| mean anomaly at epoch: | 269.0931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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