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 64020U 26145.64533059 +.00000000 +00000-0 +85764-3 0 00001
2 64020 42.9970 283.4239 0001672 198.9993 161.0796 15.27604086 09
| Epoch (UTC): | 25 May 2026 15:29:16 |
| Eccentricity: | 0.0001672 |
| inclination: | 42.9970° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 283.4239° |
| argument of perigee: | 198.9993° |
| revolutions per day: | 15.27604086 |
| mean anomaly at epoch: | 161.0796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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