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 45874U 20046B 23046.23078103 0.00085000 00000-0 39492-2 0 04
2 45874 53.9740 122.7110 0017182 197.2203 162.7796 15.19364789 06
| Epoch (UTC): | 15 February 2023 05:32:19 |
| Eccentricity: | 0.0017182 |
| inclination: | 53.9740° |
| perigee height: | 496 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 122.7110° |
| argument of perigee: | 197.2203° |
| revolutions per day: | 15.19364789 |
| mean anomaly at epoch: | 162.7796° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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