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 64217U 26143.16114603 +.00000000 +00000-0 +88685-3 0 00009
2 64217 53.1597 53.9741 0001180 86.9517 273.1619 15.30200733 00
| Epoch (UTC): | 23 May 2026 03:52:03 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.9741° |
| argument of perigee: | 86.9517° |
| revolutions per day: | 15.30200733 |
| mean anomaly at epoch: | 273.1619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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