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 39433U 26032.49131241 +.00000000 +00000-0 +13768-2 0 00000
2 39433 97.4947 42.2550 0003701 46.9670 313.1903 15.73771569 06
| Epoch (UTC): | 01 February 2026 11:47:29 |
| Eccentricity: | 0.0003701 |
| inclination: | 97.4947° |
| perigee height: | 346 km |
| apogee height: | 351 km |
| right ascension of ascending node: | 42.2550° |
| argument of perigee: | 46.9670° |
| revolutions per day: | 15.73771569 |
| mean anomaly at epoch: | 313.1903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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