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 41334U 16010A 23020.26092241 0.00000000 00000-0 00000-0 0 09
2 41334 122.9932 305.7044 0006801 145.3802 214.6198 13.41435465 03
| Epoch (UTC): | 20 January 2023 06:15:43 |
| Eccentricity: | 0.0006801 |
| inclination: | 122.9932° |
| perigee height: | 1099 km |
| apogee height: | 1109 km |
| right ascension of ascending node: | 305.7044° |
| argument of perigee: | 145.3802° |
| revolutions per day: | 13.41435465 |
| mean anomaly at epoch: | 214.6198° |
| 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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