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 00005U 58002B 23084.16015329 .00000199 00000-0 22641-3 0 9991
2 00005 34.2589 354.2815 1846661 221.2619 123.2893 10.85074623315037
| Epoch (UTC): | 25 March 2023 03:50:37 |
| Eccentricity: | 0.1846661 |
| inclination: | 34.2589° |
| perigee height: | 649 km |
| apogee height: | 3832 km |
| right ascension of ascending node: | 354.2815° |
| argument of perigee: | 221.2619° |
| revolutions per day: | 10.85074623 |
| mean anomaly at epoch: | 123.2893° |
| orbit number at epoch: | 31503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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