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 18608U 85077K 23335.38501897 .00005156 00000-0 11108-2 0 9997
2 18608 74.0488 55.1596 0011671 300.8745 59.1271 14.58659008943490
| Epoch (UTC): | 01 December 2023 09:14:25 |
| Eccentricity: | 0.0011671 |
| inclination: | 74.0488° |
| perigee height: | 689 km |
| apogee height: | 706 km |
| right ascension of ascending node: | 55.1596° |
| argument of perigee: | 300.8745° |
| revolutions per day: | 14.58659008 |
| mean anomaly at epoch: | 59.1271° |
| orbit number at epoch: | 94349 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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