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 00016U 26036.82912822 +.00000000 +00000-0 +92622-4 0 00006
2 00016 34.2812 324.8935 2022363 285.8226 52.9547 10.49576960 03
| Epoch (UTC): | 05 February 2026 19:53:56 |
| Eccentricity: | 0.2022363 |
| inclination: | 34.2812° |
| perigee height: | 652 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 324.8935° |
| argument of perigee: | 285.8226° |
| revolutions per day: | 10.49576960 |
| mean anomaly at epoch: | 52.9547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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