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 23439U 94085A 23079.84392954 -.00000039 00000-0 10000-3 0 9999
2 23439 64.8146 58.5730 0165175 225.6472 133.0817 11.27574091162653
| Epoch (UTC): | 20 March 2023 20:15:15 |
| Eccentricity: | 0.0165175 |
| inclination: | 64.8146° |
| perigee height: | 1883 km |
| apogee height: | 2161 km |
| right ascension of ascending node: | 58.5730° |
| argument of perigee: | 225.6472° |
| revolutions per day: | 11.27574091 |
| mean anomaly at epoch: | 133.0817° |
| orbit number at epoch: | 16265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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