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 64021U 26145.42732953 +.00000000 +00000-0 +11031-2 0 00007
2 64021 43.0008 284.3775 0000345 314.9287 45.1537 15.27598912 06
| Epoch (UTC): | 25 May 2026 10:15:21 |
| Eccentricity: | 0.0000345 |
| inclination: | 43.0008° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 284.3775° |
| argument of perigee: | 314.9287° |
| revolutions per day: | 15.27598912 |
| mean anomaly at epoch: | 45.1537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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