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 17369U 87011A 24282.43866741 .00000742 00000-0 31440-3 0 9998
2 17369 65.0112 175.4011 0021158 261.0939 98.7750 14.31714504 20849
| Epoch (UTC): | 08 October 2024 10:31:40 |
| Eccentricity: | 0.0021158 |
| inclination: | 65.0112° |
| perigee height: | 771 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 175.4011° |
| argument of perigee: | 261.0939° |
| revolutions per day: | 14.31714504 |
| mean anomaly at epoch: | 98.7750° |
| orbit number at epoch: | 2084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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