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 39446U 13066AG 23033.34710550 .00003600 00000-0 45646-3 0 9995
2 39446 97.7178 353.0168 0068847 60.3612 300.4434 14.80656729494467
| Epoch (UTC): | 02 February 2023 08:19:49 |
| Eccentricity: | 0.0068847 |
| inclination: | 97.7178° |
| perigee height: | 579 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 353.0168° |
| argument of perigee: | 60.3612° |
| revolutions per day: | 14.80656729 |
| mean anomaly at epoch: | 300.4434° |
| orbit number at epoch: | 49446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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