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 11963U 26088.15609891 +.00000000 +00000-0 +15028-4 0 00006
2 11963 81.2729 255.2844 0074122 358.1018 1.9859 14.10159578 06
| Epoch (UTC): | 29 March 2026 03:44:46 |
| Eccentricity: | 0.0074122 |
| inclination: | 81.2729° |
| perigee height: | 805 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 255.2844° |
| argument of perigee: | 358.1018° |
| revolutions per day: | 14.10159578 |
| mean anomaly at epoch: | 1.9859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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