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 11871U 26150.22856233 +.00000000 +00000-0 +00000-0 0 00006
2 11871 65.9495 73.9953 6636517 19.4664 356.8777 2.00970732 01
| Epoch (UTC): | 30 May 2026 05:29:07 |
| Eccentricity: | 0.6636517 |
| inclination: | 65.9495° |
| perigee height: | 2543 km |
| apogee height: | 37749 km |
| right ascension of ascending node: | 73.9953° |
| argument of perigee: | 19.4664° |
| revolutions per day: | 2.00970732 |
| mean anomaly at epoch: | 356.8777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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