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 26039.64696025 +.00000000 +00000-0 +13556-3 0 00006
2 14241 74.0571 210.8701 0017410 218.4782 141.5132 14.37506835 01
| Epoch (UTC): | 08 February 2026 15:31:37 |
| Eccentricity: | 0.0017410 |
| inclination: | 74.0571° |
| perigee height: | 754 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 210.8701° |
| argument of perigee: | 218.4782° |
| revolutions per day: | 14.37506835 |
| mean anomaly at epoch: | 141.5132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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