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 17296U 87003B 24282.42747084 .00005091 00000-0 59596-3 0 9999
2 17296 82.5306 46.4173 0019605 56.7677 303.5414 14.84745245 17928
| Epoch (UTC): | 08 October 2024 10:15:33 |
| Eccentricity: | 0.0019605 |
| inclination: | 82.5306° |
| perigee height: | 600 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 46.4173° |
| argument of perigee: | 56.7677° |
| revolutions per day: | 14.84745245 |
| mean anomaly at epoch: | 303.5414° |
| orbit number at epoch: | 1792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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