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 25338U 98030A 23090.85053212 .00000410 00000-0 18912-3 0 9990
2 25338 98.6150 121.2003 0010599 173.3666 186.7656 14.26280958294231
| Epoch (UTC): | 31 March 2023 20:24:45 |
| Eccentricity: | 0.0010599 |
| inclination: | 98.6150° |
| perigee height: | 796 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 121.2003° |
| argument of perigee: | 173.3666° |
| revolutions per day: | 14.26280958 |
| mean anomaly at epoch: | 186.7656° |
| orbit number at epoch: | 29423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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