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 64737U 26145.40913510 +.00000000 +00000-0 -11888-3 0 00001
2 64737 53.1578 184.9917 0001121 84.1497 275.9632 15.30180703 07
| Epoch (UTC): | 25 May 2026 09:49:09 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.1578° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.9917° |
| argument of perigee: | 84.1497° |
| revolutions per day: | 15.30180703 |
| mean anomaly at epoch: | 275.9632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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