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 00011U 59001A 25137.74087404 .00001994 00000-0 10434-2 0 9996
2 00011 32.8692 141.0658 1448721 327.5528 24.3513 11.89773987488343
| Epoch (UTC): | 17 May 2025 17:46:51 |
| Eccentricity: | 0.1448721 |
| inclination: | 32.8692° |
| perigee height: | 553 km |
| apogee height: | 2901 km |
| right ascension of ascending node: | 141.0658° |
| argument of perigee: | 327.5528° |
| revolutions per day: | 11.89773987 |
| mean anomaly at epoch: | 24.3513° |
| orbit number at epoch: | 48834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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