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 10114U 26039.76913042 +.00000000 +00000-0 +28732-3 0 00007
2 10114 97.5735 210.4437 0008033 35.1368 325.0408 15.44650108 02
| Epoch (UTC): | 08 February 2026 18:27:32 |
| Eccentricity: | 0.0008033 |
| inclination: | 97.5735° |
| perigee height: | 427 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 210.4437° |
| argument of perigee: | 35.1368° |
| revolutions per day: | 15.44650108 |
| mean anomaly at epoch: | 325.0408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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