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 42404U 00055SY 23080.07949167 .00013985 00000-0 16271-2 0 9995
2 42404 98.8333 21.5344 0165421 176.7635 183.4684 14.76020275376816
| Epoch (UTC): | 21 March 2023 01:54:28 |
| Eccentricity: | 0.0165421 |
| inclination: | 98.8333° |
| perigee height: | 526 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 21.5344° |
| argument of perigee: | 176.7635° |
| revolutions per day: | 14.76020275 |
| mean anomaly at epoch: | 183.4684° |
| orbit number at epoch: | 37681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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