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 59160U 26145.38815153 +.00000000 +00000-0 +72981-4 0 00007
2 59160 43.0009 34.0460 0000983 273.5098 86.5641 15.27577865 03
| Epoch (UTC): | 25 May 2026 09:18:56 |
| Eccentricity: | 0.0000983 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 34.0460° |
| argument of perigee: | 273.5098° |
| revolutions per day: | 15.27577865 |
| mean anomaly at epoch: | 86.5641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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