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 26088.22068014 +.00000000 +00000-0 +10080-3 0 00009
2 11870 74.0514 74.1587 0017037 305.3815 54.5746 14.38396671 04
| Epoch (UTC): | 29 March 2026 05:17:46 |
| Eccentricity: | 0.0017037 |
| inclination: | 74.0514° |
| perigee height: | 752 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 74.1587° |
| argument of perigee: | 305.3815° |
| revolutions per day: | 14.38396671 |
| mean anomaly at epoch: | 54.5746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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