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 11765U 26042.18587669 +.00000000 +00000-0 +32121-3 0 00009
2 11765 66.0786 219.9509 0481020 185.7739 173.7708 14.56868070 03
| Epoch (UTC): | 11 February 2026 04:27:39 |
| Eccentricity: | 0.0481020 |
| inclination: | 66.0786° |
| perigee height: | 363 km |
| apogee height: | 1044 km |
| right ascension of ascending node: | 219.9509° |
| argument of perigee: | 185.7739° |
| revolutions per day: | 14.56868070 |
| mean anomaly at epoch: | 173.7708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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