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 65447U 26145.33156986 +.00000000 +00000-0 +36474-3 0 00005
2 65447 97.4493 359.6090 0002185 82.4648 277.6827 15.05660576 04
| Epoch (UTC): | 25 May 2026 07:57:27 |
| Eccentricity: | 0.0002185 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.6090° |
| argument of perigee: | 82.4648° |
| revolutions per day: | 15.05660576 |
| mean anomaly at epoch: | 277.6827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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