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 59945U 26145.42347178 +.00000000 +00000-0 +44979-5 0 00007
2 59945 53.1594 233.3027 0000316 26.2158 333.8876 15.69699284 02
| Epoch (UTC): | 25 May 2026 10:09:47 |
| Eccentricity: | 0.0000316 |
| inclination: | 53.1594° |
| perigee height: | 360 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 233.3027° |
| argument of perigee: | 26.2158° |
| revolutions per day: | 15.69699284 |
| mean anomaly at epoch: | 333.8876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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