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 05707U 26129.47063322 +.00000000 +00000-0 +49544-4 0 00009
2 05707 74.0270 208.4941 0024406 206.6921 153.2980 14.40490942 06
| Epoch (UTC): | 09 May 2026 11:17:42 |
| Eccentricity: | 0.0024406 |
| inclination: | 74.0270° |
| perigee height: | 739 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 208.4941° |
| argument of perigee: | 206.6921° |
| revolutions per day: | 14.40490942 |
| mean anomaly at epoch: | 153.2980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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