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 64155U 26145.59720397 +.00000000 +00000-0 +15550-3 0 00003
2 64155 97.4456 196.9994 0002242 118.0867 242.0587 15.05656317 03
| Epoch (UTC): | 25 May 2026 14:19:58 |
| Eccentricity: | 0.0002242 |
| inclination: | 97.4456° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.9994° |
| argument of perigee: | 118.0867° |
| revolutions per day: | 15.05656317 |
| mean anomaly at epoch: | 242.0587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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