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 40042U 14033AJ 24262.83160199 .00016063 00000-0 11042-2 0 9990
2 40042 98.0794 231.2028 0013226 162.7225 197.4453 15.05952885557420
| Epoch (UTC): | 18 September 2024 19:57:30 |
| Eccentricity: | 0.0013226 |
| inclination: | 98.0794° |
| perigee height: | 539 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 231.2028° |
| argument of perigee: | 162.7225° |
| revolutions per day: | 15.05952885 |
| mean anomaly at epoch: | 197.4453° |
| orbit number at epoch: | 55742 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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