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 20433U 26065.32511066 +.00000000 +00000-0 +12178-3 0 00000
2 20433 74.0336 266.9025 0040327 337.9814 194.5130 14.37499407 09
| Epoch (UTC): | 06 March 2026 07:48:09 |
| Eccentricity: | 0.0040327 |
| inclination: | 74.0336° |
| perigee height: | 738 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 266.9025° |
| argument of perigee: | 337.9814° |
| revolutions per day: | 14.37499407 |
| mean anomaly at epoch: | 194.5130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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