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 20453U 90008B 23155.87143985 .00007677 00000-0 36181-3 0 9991
2 20453 35.6225 322.3647 0242258 25.0613 336.1646 14.96640842772599
| Epoch (UTC): | 04 June 2023 20:54:52 |
| Eccentricity: | 0.0242258 |
| inclination: | 35.6225° |
| perigee height: | 409 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 322.3647° |
| argument of perigee: | 25.0613° |
| revolutions per day: | 14.96640842 |
| mean anomaly at epoch: | 336.1646° |
| orbit number at epoch: | 77259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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