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 39439U 13066Z 23033.42561479 .00009116 00000-0 99978-3 0 9995
2 39439 97.6653 3.2291 0059963 5.1183 355.0633 14.86610873496180
| Epoch (UTC): | 02 February 2023 10:12:53 |
| Eccentricity: | 0.0059963 |
| inclination: | 97.6653° |
| perigee height: | 566 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 3.2291° |
| argument of perigee: | 5.1183° |
| revolutions per day: | 14.86610873 |
| mean anomaly at epoch: | 355.0633° |
| orbit number at epoch: | 49618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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