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 06323U 72104A 25118.64825715 .00000298 00000-0 10841-3 0 9999
2 06323 74.0786 140.3465 0018530 215.9273 144.0636 14.37322100739452
| Epoch (UTC): | 28 April 2025 15:33:29 |
| Eccentricity: | 0.0018530 |
| inclination: | 74.0786° |
| perigee height: | 754 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 140.3465° |
| argument of perigee: | 215.9273° |
| revolutions per day: | 14.37322100 |
| mean anomaly at epoch: | 144.0636° |
| orbit number at epoch: | 73945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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