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 65169U 26145.56377150 +.00000000 +00000-0 +11529-3 0 00003
2 65169 86.4954 259.6606 0002012 89.9221 270.2144 13.24400381 01
| Epoch (UTC): | 25 May 2026 13:31:49 |
| Eccentricity: | 0.0002012 |
| inclination: | 86.4954° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.6606° |
| argument of perigee: | 89.9221° |
| revolutions per day: | 13.24400381 |
| mean anomaly at epoch: | 270.2144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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