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 33409U 26069.84274645 +.00000000 +00000-0 +25986-3 0 00008
2 33409 97.8674 88.0916 0020066 18.4565 341.7383 15.03884973 04
| Epoch (UTC): | 10 March 2026 20:13:33 |
| Eccentricity: | 0.0020066 |
| inclination: | 97.8674° |
| perigee height: | 541 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 88.0916° |
| argument of perigee: | 18.4565° |
| revolutions per day: | 15.03884973 |
| mean anomaly at epoch: | 341.7383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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