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 11870U 26020.89559350 +.00000000 +00000-0 +21737-3 0 00007
2 11870 74.0512 198.1013 0014967 89.1964 271.0905 14.38353505 06
| Epoch (UTC): | 20 January 2026 21:29:39 |
| Eccentricity: | 0.0014967 |
| inclination: | 74.0512° |
| perigee height: | 753 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 198.1013° |
| argument of perigee: | 89.1964° |
| revolutions per day: | 14.38353505 |
| mean anomaly at epoch: | 271.0905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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