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 01328U 26162.14908412 +.00000000 +00000-0 +55306-4 0 00006
2 01328 41.1856 43.1140 0242133 274.5075 82.8058 13.38929322 02
| Epoch (UTC): | 11 June 2026 03:34:40 |
| Eccentricity: | 0.0242133 |
| inclination: | 41.1856° |
| perigee height: | 932 km |
| apogee height: | 1295 km |
| right ascension of ascending node: | 43.1140° |
| argument of perigee: | 274.5075° |
| revolutions per day: | 13.38929322 |
| mean anomaly at epoch: | 82.8058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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