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 9903U 77024A 23150.42132544 .00000230 00000-0 12628-3 0 9994
2 9903 81.2701 135.4827 0036597 273.1463 86.5519 14.08466312370962
| Epoch (UTC): | 30 May 2023 10:06:42 |
| Eccentricity: | 0.0036597 |
| inclination: | 81.2701° |
| perigee height: | 838 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 135.4827° |
| argument of perigee: | 273.1463° |
| revolutions per day: | 14.08466312 |
| mean anomaly at epoch: | 86.5519° |
| orbit number at epoch: | 37096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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