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 27433U 02024D 25108.52277047 .00000698 00000-0 38898-3 0 9999
2 27433 98.9730 151.4343 0013113 263.5533 96.4147 14.14269536181310
| Epoch (UTC): | 18 April 2025 12:32:47 |
| Eccentricity: | 0.0013113 |
| inclination: | 98.9730° |
| perigee height: | 835 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 151.4343° |
| argument of perigee: | 263.5533° |
| revolutions per day: | 14.14269536 |
| mean anomaly at epoch: | 96.4147° |
| orbit number at epoch: | 18131 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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