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 23332.86527352 .00000200 00000-0 15252-3 0 9995
2 00059 28.2470 228.6421 0189014 57.2075 304.6529 13.53049258116932
| Epoch (UTC): | 28 November 2023 20:45:59 |
| Eccentricity: | 0.0189014 |
| inclination: | 28.2470° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 228.6421° |
| argument of perigee: | 57.2075° |
| revolutions per day: | 13.53049258 |
| mean anomaly at epoch: | 304.6529° |
| orbit number at epoch: | 11693 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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