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 64917U 26144.98151016 +.00000000 +00000-0 +96478-3 0 00005
2 64917 53.1605 351.3506 0001232 86.4550 273.6592 15.31716096 01
| Epoch (UTC): | 24 May 2026 23:33:22 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 351.3506° |
| argument of perigee: | 86.4550° |
| revolutions per day: | 15.31716096 |
| mean anomaly at epoch: | 273.6592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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