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 26106.26947819 +.00000000 +00000-0 +43228-4 0 00001
2 01328 41.1841 282.2155 0241916 343.7502 15.5597 13.38923411 04
| Epoch (UTC): | 16 April 2026 06:28:02 |
| Eccentricity: | 0.0241916 |
| inclination: | 41.1841° |
| perigee height: | 932 km |
| apogee height: | 1295 km |
| right ascension of ascending node: | 282.2155° |
| argument of perigee: | 343.7502° |
| revolutions per day: | 13.38923411 |
| mean anomaly at epoch: | 15.5597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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