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 64151U 26145.38675029 +.00000000 +00000-0 +19525-3 0 00003
2 64151 97.4473 196.8155 0001742 146.7367 213.3970 15.05658250 08
| Epoch (UTC): | 25 May 2026 09:16:55 |
| Eccentricity: | 0.0001742 |
| inclination: | 97.4473° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.8155° |
| argument of perigee: | 146.7367° |
| revolutions per day: | 15.05658250 |
| mean anomaly at epoch: | 213.3970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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