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 64907U 26144.99654036 +.00000000 +00000-0 +97219-3 0 00009
2 64907 53.1606 350.0348 0001435 103.0031 257.1132 15.34401520 09
| Epoch (UTC): | 24 May 2026 23:55:01 |
| Eccentricity: | 0.0001435 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 350.0348° |
| argument of perigee: | 103.0031° |
| revolutions per day: | 15.34401520 |
| mean anomaly at epoch: | 257.1132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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