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 64033U 26145.39821237 +.00000000 +00000-0 +10028-3 0 00006
2 64033 69.9999 280.9890 0003657 264.8949 95.1793 14.98330602 08
| Epoch (UTC): | 25 May 2026 09:33:25 |
| Eccentricity: | 0.0003657 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 280.9890° |
| argument of perigee: | 264.8949° |
| revolutions per day: | 14.98330602 |
| mean anomaly at epoch: | 95.1793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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