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 25339.14734689 .00000149 00000-0 10028-3 0 9998
2 27432 98.9010 27.9451 0049211 291.9022 127.3136 14.14525459215873
| Epoch (UTC): | 05 December 2025 03:32:10 |
| Eccentricity: | 0.0049211 |
| inclination: | 98.9010° |
| perigee height: | 808 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 27.9451° |
| argument of perigee: | 291.9022° |
| revolutions per day: | 14.14525459 |
| mean anomaly at epoch: | 127.3136° |
| orbit number at epoch: | 21587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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