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 39440U 13066AA 22176.85611227 .00001242 00000-0 17406-3 0 9996
2 39440 97.7263 134.0596 0080278 103.8648 257.1510 14.77025339461529
| Epoch (UTC): | 25 June 2022 20:32:48 |
| Eccentricity: | 0.0080278 |
| inclination: | 97.7263° |
| perigee height: | 582 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 134.0596° |
| argument of perigee: | 103.8648° |
| revolutions per day: | 14.77025339 |
| mean anomaly at epoch: | 257.1510° |
| orbit number at epoch: | 46152 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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