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 65064U 26145.45499448 +.00000000 +00000-0 +33874-3 0 00007
2 65064 97.4478 222.5552 0002419 144.7299 215.4089 15.05654146 03
| Epoch (UTC): | 25 May 2026 10:55:11 |
| Eccentricity: | 0.0002419 |
| inclination: | 97.4478° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.5552° |
| argument of perigee: | 144.7299° |
| revolutions per day: | 15.05654146 |
| mean anomaly at epoch: | 215.4089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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