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 23266.24106475 .00000132 00000-0 53391-4 0 9993
2 00059 28.2479 210.9108 0189154 217.8874 140.8224 13.53040383107902
| Epoch (UTC): | 23 September 2023 05:47:07 |
| Eccentricity: | 0.0189154 |
| inclination: | 28.2479° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 210.9108° |
| argument of perigee: | 217.8874° |
| revolutions per day: | 13.53040383 |
| mean anomaly at epoch: | 140.8224° |
| orbit number at epoch: | 10790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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