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 00045U 60007A 24262.32000942 .00001308 00000-0 33998-3 0 9995
2 00045 66.6918 243.6752 0259202 264.1091 93.0413 14.34938354288630
| Epoch (UTC): | 18 September 2024 07:40:48 |
| Eccentricity: | 0.0259202 |
| inclination: | 66.6918° |
| perigee height: | 590 km |
| apogee height: | 960 km |
| right ascension of ascending node: | 243.6752° |
| argument of perigee: | 264.1091° |
| revolutions per day: | 14.34938354 |
| mean anomaly at epoch: | 93.0413° |
| orbit number at epoch: | 28863 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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