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 5U 58002B 23089.03782561 .00000151 00000-0 16406-3 0 9991
2 5 34.2620 339.2527 1846928 243.2130 96.8045 10.85076028315657
| Epoch (UTC): | 30 March 2023 00:54:28 |
| Eccentricity: | 0.1846928 |
| inclination: | 34.2620° |
| perigee height: | 648 km |
| apogee height: | 3832 km |
| right ascension of ascending node: | 339.2527° |
| argument of perigee: | 243.2130° |
| revolutions per day: | 10.85076028 |
| mean anomaly at epoch: | 96.8045° |
| orbit number at epoch: | 31565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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