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 17528U 87018B 24276.61254435 .00003532 00000-0 74891-3 0 9993
2 17528 97.4513 330.2513 0146171 221.6012 137.3993 14.53215684965728
| Epoch (UTC): | 02 October 2024 14:42:03 |
| Eccentricity: | 0.0146171 |
| inclination: | 97.4513° |
| perigee height: | 611 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 330.2513° |
| argument of perigee: | 221.6012° |
| revolutions per day: | 14.53215684 |
| mean anomaly at epoch: | 137.3993° |
| orbit number at epoch: | 96572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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