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 39427U 13066M 25143.82835415 .00002958 00000-0 37768-3 0 9990
2 39427 97.8382 58.0266 0096240 61.2800 299.8042 14.78948130616674
| Epoch (UTC): | 23 May 2025 19:52:49 |
| Eccentricity: | 0.0096240 |
| inclination: | 97.8382° |
| perigee height: | 565 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 58.0266° |
| argument of perigee: | 61.2800° |
| revolutions per day: | 14.78948130 |
| mean anomaly at epoch: | 299.8042° |
| orbit number at epoch: | 61667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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