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 14452U 26039.16128663 +.00000000 +00000-0 +79945-4 0 00000
2 14452 81.1624 127.4482 0089466 216.8137 142.6881 14.27239536 01
| Epoch (UTC): | 08 February 2026 03:52:15 |
| Eccentricity: | 0.0089466 |
| inclination: | 81.1624° |
| perigee height: | 737 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 127.4482° |
| argument of perigee: | 216.8137° |
| revolutions per day: | 14.27239536 |
| mean anomaly at epoch: | 142.6881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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