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 64218U 26145.13841557 +.00000000 +00000-0 +55029-3 0 00000
2 64218 53.1586 44.2760 0001064 92.5600 267.5523 15.30212669 02
| Epoch (UTC): | 25 May 2026 03:19:19 |
| Eccentricity: | 0.0001064 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.2760° |
| argument of perigee: | 92.5600° |
| revolutions per day: | 15.30212669 |
| mean anomaly at epoch: | 267.5523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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