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 28395U 04031C 23342.55994452 .00006561 00000-0 12181-2 0 9995
2 28395 49.3843 102.6562 5216439 157.6076 237.7894 5.25885784355649
| Epoch (UTC): | 08 December 2023 13:26:19 |
| Eccentricity: | 0.5216439 |
| inclination: | 49.3843° |
| perigee height: | 303 km |
| apogee height: | 14876 km |
| right ascension of ascending node: | 102.6562° |
| argument of perigee: | 157.6076° |
| revolutions per day: | 5.25885784 |
| mean anomaly at epoch: | 237.7894° |
| orbit number at epoch: | 35564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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