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 00059U 60013B 23036.93040083 .00000153 00000-0 88852-4 0 9999
2 00059 28.2486 308.9344 0189177 93.1224 269.0983 13.53017400 76825
| Epoch (UTC): | 05 February 2023 22:19:46 |
| Eccentricity: | 0.0189177 |
| inclination: | 28.2486° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 308.9344° |
| argument of perigee: | 93.1224° |
| revolutions per day: | 13.53017400 |
| mean anomaly at epoch: | 269.0983° |
| orbit number at epoch: | 7682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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