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 14241U 26040.27329742 +.00000000 +00000-0 +13804-3 0 00002
2 14241 74.0571 209.7190 0017416 217.3221 142.6724 14.37507366 01
| Epoch (UTC): | 09 February 2026 06:33:32 |
| Eccentricity: | 0.0017416 |
| inclination: | 74.0571° |
| perigee height: | 754 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 209.7190° |
| argument of perigee: | 217.3221° |
| revolutions per day: | 14.37507366 |
| mean anomaly at epoch: | 142.6724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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