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 24258.34713509 .00002344 00000-0 58799-3 0 9999
2 00045 66.6929 254.1685 0259300 266.9313 90.2092 14.34928522288065
| Epoch (UTC): | 14 September 2024 08:19:52 |
| Eccentricity: | 0.0259300 |
| inclination: | 66.6929° |
| perigee height: | 590 km |
| apogee height: | 961 km |
| right ascension of ascending node: | 254.1685° |
| argument of perigee: | 266.9313° |
| revolutions per day: | 14.34928522 |
| mean anomaly at epoch: | 90.2092° |
| orbit number at epoch: | 28806 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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