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 64113U 26144.96404985 +.00000000 +00000-0 +61014-3 0 00005
2 64113 53.1597 32.2456 0000976 81.2711 278.8401 15.31709953 04
| Epoch (UTC): | 24 May 2026 23:08:13 |
| Eccentricity: | 0.0000976 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 32.2456° |
| argument of perigee: | 81.2711° |
| revolutions per day: | 15.31709953 |
| mean anomaly at epoch: | 278.8401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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