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 58U 60013A 23337.81425855 .00000123 00000-0 60145-4 0 9995
2 58 28.3247 160.0691 0164800 97.2451 264.6858 13.46363132109664
| Epoch (UTC): | 03 December 2023 19:32:31 |
| Eccentricity: | 0.0164800 |
| inclination: | 28.3247° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 160.0691° |
| argument of perigee: | 97.2451° |
| revolutions per day: | 13.46363132 |
| mean anomaly at epoch: | 264.6858° |
| orbit number at epoch: | 10966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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