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 64869U 26145.55892506 +.00000000 +00000-0 +21863-3 0 00007
2 64869 97.6729 209.9018 0004088 318.2843 41.8065 14.94183197 04
| Epoch (UTC): | 25 May 2026 13:24:51 |
| Eccentricity: | 0.0004088 |
| inclination: | 97.6729° |
| perigee height: | 582 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 209.9018° |
| argument of perigee: | 318.2843° |
| revolutions per day: | 14.94183197 |
| mean anomaly at epoch: | 41.8065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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