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 21418U 91041A 24276.60450853 .00000839 00000-0 31994-3 0 9992
2 21418 74.0372 168.8220 0016025 110.4748 249.8125 14.32282718739836
| Epoch (UTC): | 02 October 2024 14:30:29 |
| Eccentricity: | 0.0016025 |
| inclination: | 74.0372° |
| perigee height: | 772 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 168.8220° |
| argument of perigee: | 110.4748° |
| revolutions per day: | 14.32282718 |
| mean anomaly at epoch: | 249.8125° |
| orbit number at epoch: | 73983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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