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 27432U 02024C 25140.60497959 .00000042 00000-0 44666-4 0 9993
2 27432 98.9251 189.7330 0051030 134.0846 350.6203 14.14481364187809
| Epoch (UTC): | 20 May 2025 14:31:10 |
| Eccentricity: | 0.0051030 |
| inclination: | 98.9251° |
| perigee height: | 807 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 189.7330° |
| argument of perigee: | 134.0846° |
| revolutions per day: | 14.14481364 |
| mean anomaly at epoch: | 350.6203° |
| orbit number at epoch: | 18780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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