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 64320U 26144.75665502 +.00000000 +00000-0 +15719-2 0 00006
2 64320 42.9980 291.0752 0001277 300.4114 59.6627 15.70881331 07
| Epoch (UTC): | 24 May 2026 18:09:34 |
| Eccentricity: | 0.0001277 |
| inclination: | 42.9980° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 291.0752° |
| argument of perigee: | 300.4114° |
| revolutions per day: | 15.70881331 |
| mean anomaly at epoch: | 59.6627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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