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 64799U 26145.41530163 +.00000000 +00000-0 +40503-3 0 00004
2 64799 70.0007 300.8410 0002335 267.3588 92.7303 14.98350255 05
| Epoch (UTC): | 25 May 2026 09:58:02 |
| Eccentricity: | 0.0002335 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8410° |
| argument of perigee: | 267.3588° |
| revolutions per day: | 14.98350255 |
| mean anomaly at epoch: | 92.7303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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