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 64824U 26145.47666593 +.00000000 +00000-0 +45674-3 0 00000
2 64824 51.9026 318.5579 0000682 118.1097 241.9935 14.79937015 09
| Epoch (UTC): | 25 May 2026 11:26:23 |
| Eccentricity: | 0.0000682 |
| inclination: | 51.9026° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 318.5579° |
| argument of perigee: | 118.1097° |
| revolutions per day: | 14.79937015 |
| mean anomaly at epoch: | 241.9935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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