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 23080.90821021 -.00000039 00000-0 10000-3 0 9990
2 23439 64.8144 56.8516 0165151 225.4540 133.2795 11.27574073162772
| Epoch (UTC): | 21 March 2023 21:47:49 |
| Eccentricity: | 0.0165151 |
| inclination: | 64.8144° |
| perigee height: | 1883 km |
| apogee height: | 2161 km |
| right ascension of ascending node: | 56.8516° |
| argument of perigee: | 225.4540° |
| revolutions per day: | 11.27574073 |
| mean anomaly at epoch: | 133.2795° |
| orbit number at epoch: | 16277 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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