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 64602U 26145.24098295 +.00000000 +00000-0 +11414-2 0 00001
2 64602 53.1593 339.7756 0000940 82.6454 277.4654 15.30212662 01
| Epoch (UTC): | 25 May 2026 05:47:00 |
| Eccentricity: | 0.0000940 |
| inclination: | 53.1593° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.7756° |
| argument of perigee: | 82.6454° |
| revolutions per day: | 15.30212662 |
| mean anomaly at epoch: | 277.4654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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