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 13083U 26150.61475986 +.00000000 +00000-0 +00000-0 0 00008
2 13083 11.3929 327.6930 0012834 214.1612 135.2951 0.99225874 09
| Epoch (UTC): | 30 May 2026 14:45:15 |
| Eccentricity: | 0.0012834 |
| inclination: | 11.3929° |
| perigee height: | 36028 km |
| apogee height: | 36137 km |
| right ascension of ascending node: | 327.6930° |
| argument of perigee: | 214.1612° |
| revolutions per day: | 0.99225874 |
| mean anomaly at epoch: | 135.2951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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