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 17974U 26040.59838334 +.00000000 +00000-0 -24976-4 0 00009
2 17974 71.0073 92.0570 0016128 251.1398 221.2564 14.17638852 05
| Epoch (UTC): | 09 February 2026 14:21:40 |
| Eccentricity: | 0.0016128 |
| inclination: | 71.0073° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 92.0570° |
| argument of perigee: | 251.1398° |
| revolutions per day: | 14.17638852 |
| mean anomaly at epoch: | 221.2564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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