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 59096U 26145.52812275 +.00000000 +00000-0 +52705-4 0 00005
2 59096 43.0001 236.6960 0000752 257.0607 103.0160 15.27581327 04
| Epoch (UTC): | 25 May 2026 12:40:29 |
| Eccentricity: | 0.0000752 |
| inclination: | 43.0001° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.6960° |
| argument of perigee: | 257.0607° |
| revolutions per day: | 15.27581327 |
| mean anomaly at epoch: | 103.0160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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