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 21135.77810375 .00000057 00000-0 28363-4 0 9993
2 20433 74.0363 253.2468 0040405 32.7737 76.8085 14.36135323639990
| Epoch (UTC): | 15 May 2021 18:40:28 |
| Eccentricity: | 0.0040405 |
| inclination: | 74.0363° |
| perigee height: | 742 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 253.2468° |
| argument of perigee: | 32.7737° |
| revolutions per day: | 14.36135323 |
| mean anomaly at epoch: | 76.8085° |
| orbit number at epoch: | 63999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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