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 26020.99938566 +.00000000 +00000-0 +39840-3 0 00004
2 33409 97.8652 38.4396 0019728 174.6427 185.5013 15.03533629 09
| Epoch (UTC): | 20 January 2026 23:59:06 |
| Eccentricity: | 0.0019728 |
| inclination: | 97.8652° |
| perigee height: | 542 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 38.4396° |
| argument of perigee: | 174.6427° |
| revolutions per day: | 15.03533629 |
| mean anomaly at epoch: | 185.5013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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