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 26073.58495483 +.00000000 +00000-0 +12140-3 0 00000
2 20433 74.0339 251.6995 0040624 321.0256 99.0262 14.37505519 00
| Epoch (UTC): | 14 March 2026 14:02:20 |
| Eccentricity: | 0.0040624 |
| inclination: | 74.0339° |
| perigee height: | 738 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 251.6995° |
| argument of perigee: | 321.0256° |
| revolutions per day: | 14.37505519 |
| mean anomaly at epoch: | 99.0262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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