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 64330U 26145.42226940 +.00000000 +00000-0 +69580-3 0 00007
2 64330 42.9970 48.5429 0000912 59.2049 300.8893 15.27577313 04
| Epoch (UTC): | 25 May 2026 10:08:04 |
| Eccentricity: | 0.0000912 |
| inclination: | 42.9970° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.5429° |
| argument of perigee: | 59.2049° |
| revolutions per day: | 15.27577313 |
| mean anomaly at epoch: | 300.8893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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