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 59105U 26145.33002300 +.00000000 +00000-0 +17190-3 0 00003
2 59105 97.8361 275.9172 0007543 110.2733 249.9300 14.97084662 09
| Epoch (UTC): | 25 May 2026 07:55:13 |
| Eccentricity: | 0.0007543 |
| inclination: | 97.8361° |
| perigee height: | 571 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 275.9172° |
| argument of perigee: | 110.2733° |
| revolutions per day: | 14.97084662 |
| mean anomaly at epoch: | 249.9300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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