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 65939U 26145.62783337 +.00000000 +00000-0 +24404-3 0 00009
2 65939 97.6395 224.3092 0018199 208.0720 151.9529 15.10322166 01
| Epoch (UTC): | 25 May 2026 15:04:04 |
| Eccentricity: | 0.0018199 |
| inclination: | 97.6395° |
| perigee height: | 523 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 224.3092° |
| argument of perigee: | 208.0720° |
| revolutions per day: | 15.10322166 |
| mean anomaly at epoch: | 151.9529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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