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 64872U 26145.65440899 +.00000000 +00000-0 +55797-3 0 00009
2 64872 97.6668 210.6930 0003846 352.9814 7.1354 14.97310459 08
| Epoch (UTC): | 25 May 2026 15:42:20 |
| Eccentricity: | 0.0003846 |
| inclination: | 97.6668° |
| perigee height: | 573 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 210.6930° |
| argument of perigee: | 352.9814° |
| revolutions per day: | 14.97310459 |
| mean anomaly at epoch: | 7.1354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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