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 64622U 26145.43419078 +.00000000 +00000-0 +18490-3 0 00002
2 64622 97.4469 148.8824 0012013 210.4164 149.6375 15.18003512 02
| Epoch (UTC): | 25 May 2026 10:25:14 |
| Eccentricity: | 0.0012013 |
| inclination: | 97.4469° |
| perigee height: | 504 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 148.8824° |
| argument of perigee: | 210.4164° |
| revolutions per day: | 15.18003512 |
| mean anomaly at epoch: | 149.6375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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