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 24280.72036204 .00001640 00000-0 41962-3 0 9998
2 00045 66.6942 195.0796 0258665 251.0335 106.2575 14.34987986291278
| Epoch (UTC): | 06 October 2024 17:17:19 |
| Eccentricity: | 0.0258665 |
| inclination: | 66.6942° |
| perigee height: | 590 km |
| apogee height: | 960 km |
| right ascension of ascending node: | 195.0796° |
| argument of perigee: | 251.0335° |
| revolutions per day: | 14.34987986 |
| mean anomaly at epoch: | 106.2575° |
| orbit number at epoch: | 29127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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