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 39442U 13066AC 25073.51537644 .00026140 00000-0 13897-2 0 9993
2 39442 97.5513 58.7146 0024833 110.9493 249.4400 15.14984318614268
| Epoch (UTC): | 14 March 2025 12:22:08 |
| Eccentricity: | 0.0024833 |
| inclination: | 97.5513° |
| perigee height: | 504 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 58.7146° |
| argument of perigee: | 110.9493° |
| revolutions per day: | 15.14984318 |
| mean anomaly at epoch: | 249.4400° |
| orbit number at epoch: | 61426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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