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 53807U 22111AL 23152.38089501 .00004899 00000-0 23403-3 0 9992
2 53807 53.1967 145.5793 0013225 4.8205 355.2917 15.20737463 40040
| Epoch (UTC): | 01 June 2023 09:08:29 |
| Eccentricity: | 0.0013225 |
| inclination: | 53.1967° |
| perigee height: | 494 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 145.5793° |
| argument of perigee: | 4.8205° |
| revolutions per day: | 15.20737463 |
| mean anomaly at epoch: | 355.2917° |
| orbit number at epoch: | 4004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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