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 64772U 26145.57671513 +.00000000 +00000-0 +73655-3 0 00001
2 64772 53.1583 244.8973 0000112 207.3575 152.7422 15.34402008 03
| Epoch (UTC): | 25 May 2026 13:50:28 |
| Eccentricity: | 0.0000112 |
| inclination: | 53.1583° |
| perigee height: | 463 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 244.8973° |
| argument of perigee: | 207.3575° |
| revolutions per day: | 15.34402008 |
| mean anomaly at epoch: | 152.7422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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