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 00082U 26133.38149521 +.00000000 +00000-0 +12983-3 0 00007
2 00082 38.8523 129.0712 1166046 57.5584 313.2541 12.27901976 04
| Epoch (UTC): | 13 May 2026 09:09:21 |
| Eccentricity: | 0.1166046 |
| inclination: | 38.8523° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 129.0712° |
| argument of perigee: | 57.5584° |
| revolutions per day: | 12.27901976 |
| mean anomaly at epoch: | 313.2541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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