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 data is extracted from the following two-line orbital elements,
1 20433U 90004B 23150.78414737 .00000272 00000-0 10076-3 0 9995
2 20433 74.0360 325.0282 0041504 283.8770 86.8572 14.36450583747233
| Epoch (UTC): | 30 May 2023 18:49:10 |
| Eccentricity: | 0.0041504 |
| inclination: | 74.0360° |
| perigee height: | 740 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 325.0282° |
| argument of perigee: | 283.8770° |
| revolutions per day: | 14.36450583 |
| mean anomaly at epoch: | 86.8572° |
| orbit number at epoch: | 74723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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