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 10516U 26150.51553816 +.00000000 +00000-0 +00000-0 0 00004
2 10516 7.4195 297.2270 0002268 107.1436 165.6238 0.98916563 08
| Epoch (UTC): | 30 May 2026 12:22:22 |
| Eccentricity: | 0.0002268 |
| inclination: | 7.4195° |
| perigee height: | 36161 km |
| apogee height: | 36181 km |
| right ascension of ascending node: | 297.2270° |
| argument of perigee: | 107.1436° |
| revolutions per day: | 0.98916563 |
| mean anomaly at epoch: | 165.6238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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