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 24288.58102559 .00000250 00000-0 21017-3 0 9994
2 00059 28.2507 20.9375 0188887 229.4956 128.8991 13.53099392160406
| Epoch (UTC): | 14 October 2024 13:56:40 |
| Eccentricity: | 0.0188887 |
| inclination: | 28.2507° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 20.9375° |
| argument of perigee: | 229.4956° |
| revolutions per day: | 13.53099392 |
| mean anomaly at epoch: | 128.8991° |
| orbit number at epoch: | 16040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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