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 23080.20336065 .00000105 00000-0 11393-3 0 9994
2 00005 34.2555 6.4755 1846371 203.4491 147.0052 10.85073108314607
| Epoch (UTC): | 21 March 2023 04:52:50 |
| Eccentricity: | 0.1846371 |
| inclination: | 34.2555° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 6.4755° |
| argument of perigee: | 203.4491° |
| revolutions per day: | 10.85073108 |
| mean anomaly at epoch: | 147.0052° |
| orbit number at epoch: | 31460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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