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 26020.20007344 +.00000000 +00000-0 +16813-3 0 00002
2 11870 74.0513 199.3817 0014958 90.7318 269.5550 14.38351882 07
| Epoch (UTC): | 20 January 2026 04:48:06 |
| Eccentricity: | 0.0014958 |
| inclination: | 74.0513° |
| perigee height: | 753 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 199.3817° |
| argument of perigee: | 90.7318° |
| revolutions per day: | 14.38351882 |
| mean anomaly at epoch: | 269.5550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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