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 64360U 26145.40998832 +.00000000 +00000-0 +21735-2 0 00003
2 64360 70.0000 201.0207 0003706 280.7236 79.3506 14.98307669 07
| Epoch (UTC): | 25 May 2026 09:50:22 |
| Eccentricity: | 0.0003706 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.0207° |
| argument of perigee: | 280.7236° |
| revolutions per day: | 14.98307669 |
| mean anomaly at epoch: | 79.3506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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