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 23657U 95046A 23276.45505531 .00003255 00000-0 34674-3 0 9997
2 23657 82.5237 258.8851 0021786 28.8576 331.3842 14.88460375519037
| Epoch (UTC): | 03 October 2023 10:55:16 |
| Eccentricity: | 0.0021786 |
| inclination: | 82.5237° |
| perigee height: | 587 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 258.8851° |
| argument of perigee: | 28.8576° |
| revolutions per day: | 14.88460375 |
| mean anomaly at epoch: | 331.3842° |
| orbit number at epoch: | 51903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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