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 23339.87439747 .00000151 00000-0 84871-4 0 9992
2 00059 28.2458 192.6315 0189046 116.0522 245.9614 13.53050518117884
| Epoch (UTC): | 05 December 2023 20:59:07 |
| Eccentricity: | 0.0189046 |
| inclination: | 28.2458° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 192.6315° |
| argument of perigee: | 116.0522° |
| revolutions per day: | 13.53050518 |
| mean anomaly at epoch: | 245.9614° |
| orbit number at epoch: | 11788 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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