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 00059U 60013B 23089.53619298 .00000134 00000-0 58112-4 0 9998
2 00059 28.2499 38.6825 0189230 174.6418 185.6199 13.53024941 83952
| Epoch (UTC): | 30 March 2023 12:52:07 |
| Eccentricity: | 0.0189230 |
| inclination: | 28.2499° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 38.6825° |
| argument of perigee: | 174.6418° |
| revolutions per day: | 13.53024941 |
| mean anomaly at epoch: | 185.6199° |
| orbit number at epoch: | 8395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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