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 23545U 95017A 24357.85255139 .00011910 00000-0 13641-2 0 9999
2 23545 69.9641 152.6672 0006634 251.5400 108.5032 14.86096092586273
| Epoch (UTC): | 22 December 2024 20:27:40 |
| Eccentricity: | 0.0006634 |
| inclination: | 69.9641° |
| perigee height: | 605 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 152.6672° |
| argument of perigee: | 251.5400° |
| revolutions per day: | 14.86096092 |
| mean anomaly at epoch: | 108.5032° |
| orbit number at epoch: | 58627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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