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 00046U 60007B 23032.46413384 .00000505 00000-0 12250-3 0 9999
2 00046 66.6918 334.2602 0202936 137.5066 224.1956 14.50071963278101
| Epoch (UTC): | 01 February 2023 11:08:21 |
| Eccentricity: | 0.0202936 |
| inclination: | 66.6918° |
| perigee height: | 581 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 334.2602° |
| argument of perigee: | 137.5066° |
| revolutions per day: | 14.50071963 |
| mean anomaly at epoch: | 224.1956° |
| orbit number at epoch: | 27810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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