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 65526U 26145.44744699 +.00000000 +00000-0 +19603-3 0 00004
2 65526 97.4457 215.1299 0003078 131.2905 228.8588 15.05654858 08
| Epoch (UTC): | 25 May 2026 10:44:19 |
| Eccentricity: | 0.0003078 |
| inclination: | 97.4457° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 215.1299° |
| argument of perigee: | 131.2905° |
| revolutions per day: | 15.05654858 |
| mean anomaly at epoch: | 228.8588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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