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 23027.29120186 .00000723 00000-0 16533-3 0 9999
2 00046 66.6915 348.2533 0203353 141.4646 220.1183 14.50064802277356
| Epoch (UTC): | 27 January 2023 06:59:19 |
| Eccentricity: | 0.0203353 |
| inclination: | 66.6915° |
| perigee height: | 581 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 348.2533° |
| argument of perigee: | 141.4646° |
| revolutions per day: | 14.50064802 |
| mean anomaly at epoch: | 220.1183° |
| orbit number at epoch: | 27735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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