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 64536U 26145.23540476 +.00000000 +00000-0 +11689-3 0 00004
2 64536 97.4622 259.8097 0002629 260.3129 99.7809 15.19824914 04
| Epoch (UTC): | 25 May 2026 05:38:58 |
| Eccentricity: | 0.0002629 |
| inclination: | 97.4622° |
| perigee height: | 505 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 259.8097° |
| argument of perigee: | 260.3129° |
| revolutions per day: | 15.19824914 |
| mean anomaly at epoch: | 99.7809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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