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 26076.32763041 +.00000000 +00000-0 +74565-4 0 00008
2 11870 74.0507 96.0574 0016666 329.0150 31.0020 14.38390673 08
| Epoch (UTC): | 17 March 2026 07:51:47 |
| Eccentricity: | 0.0016666 |
| inclination: | 74.0507° |
| perigee height: | 752 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 96.0574° |
| argument of perigee: | 329.0150° |
| revolutions per day: | 14.38390673 |
| mean anomaly at epoch: | 31.0020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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