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 64393U 26144.76324301 +.00000000 +00000-0 +10121-5 0 00001
2 64393 97.3568 272.0944 0012691 188.9851 171.1160 15.20970536 07
| Epoch (UTC): | 24 May 2026 18:19:04 |
| Eccentricity: | 0.0012691 |
| inclination: | 97.3568° |
| perigee height: | 494 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 272.0944° |
| argument of perigee: | 188.9851° |
| revolutions per day: | 15.20970536 |
| mean anomaly at epoch: | 171.1160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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