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 32105U 99025CQX 24351.88702798 .00003397 00000-0 41347-2 0 9993
2 32105 103.4595 220.2116 0399562 105.1997 259.3656 13.37994959844067
| Epoch (UTC): | 16 December 2024 21:17:19 |
| Eccentricity: | 0.0399562 |
| inclination: | 103.4595° |
| perigee height: | 817 km |
| apogee height: | 1416 km |
| right ascension of ascending node: | 220.2116° |
| argument of perigee: | 105.1997° |
| revolutions per day: | 13.37994959 |
| mean anomaly at epoch: | 259.3656° |
| orbit number at epoch: | 84406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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