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 00045U 60007A 23331.32046341 .00000391 00000-0 12494-3 0 9993
2 00045 66.6940 304.9400 0246787 120.6317 241.9369 14.34449505246179
| Epoch (UTC): | 27 November 2023 07:41:28 |
| Eccentricity: | 0.0246787 |
| inclination: | 66.6940° |
| perigee height: | 600 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 304.9400° |
| argument of perigee: | 120.6317° |
| revolutions per day: | 14.34449505 |
| mean anomaly at epoch: | 241.9369° |
| orbit number at epoch: | 24617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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