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 48732U 02032BR 23032.40081138 .00007190 00000-0 21582-2 0 9993
2 48732 98.7102 358.7570 0045600 116.1620 244.4269 14.42410699 97894
| Epoch (UTC): | 01 February 2023 09:37:10 |
| Eccentricity: | 0.0045600 |
| inclination: | 98.7102° |
| perigee height: | 718 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 358.7570° |
| argument of perigee: | 116.1620° |
| revolutions per day: | 14.42410699 |
| mean anomaly at epoch: | 244.4269° |
| orbit number at epoch: | 9789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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