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 59225U 24047B 24357.91116216 .00019794 00000-0 11951-2 0 9997
2 59225 97.5903 321.8257 0014937 92.2643 268.0297 15.10650725 42907
| Epoch (UTC): | 22 December 2024 21:52:04 |
| Eccentricity: | 0.0014937 |
| inclination: | 97.5903° |
| perigee height: | 524 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 321.8257° |
| argument of perigee: | 92.2643° |
| revolutions per day: | 15.10650725 |
| mean anomaly at epoch: | 268.0297° |
| orbit number at epoch: | 4290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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