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 27422U 02021B 23083.42771857 .00001682 00000-0 67265-3 0 9995
2 27422 98.4835 26.5138 0012988 127.7304 232.5058 14.29628076 87558
| Epoch (UTC): | 24 March 2023 10:15:54 |
| Eccentricity: | 0.0012988 |
| inclination: | 98.4835° |
| perigee height: | 783 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 26.5138° |
| argument of perigee: | 127.7304° |
| revolutions per day: | 14.29628076 |
| mean anomaly at epoch: | 232.5058° |
| orbit number at epoch: | 8755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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