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 48635U 21006FB 23033.08554926 .00060432 00000-0 15877-2 0 9990
2 48635 97.1779 78.2741 0009855 155.0113 205.1612 15.38348803112442
| Epoch (UTC): | 02 February 2023 02:03:11 |
| Eccentricity: | 0.0009855 |
| inclination: | 97.1779° |
| perigee height: | 444 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 78.2741° |
| argument of perigee: | 155.0113° |
| revolutions per day: | 15.38348803 |
| mean anomaly at epoch: | 205.1612° |
| orbit number at epoch: | 11244 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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