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 64299U 26145.56208764 +.00000000 +00000-0 +11538-3 0 00000
2 64299 70.0048 0.6247 0003102 302.0941 57.9917 14.98327143 05
| Epoch (UTC): | 25 May 2026 13:29:24 |
| Eccentricity: | 0.0003102 |
| inclination: | 70.0048° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 0.6247° |
| argument of perigee: | 302.0941° |
| revolutions per day: | 14.98327143 |
| mean anomaly at epoch: | 57.9917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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