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 23340.59250654 -.00000048 00000-0 -16934-3 0 9995
2 23439 64.8195 356.8542 0156713 179.6874 180.4173 11.27575489191761
| Epoch (UTC): | 06 December 2023 14:13:12 |
| Eccentricity: | 0.0156713 |
| inclination: | 64.8195° |
| perigee height: | 1891 km |
| apogee height: | 2154 km |
| right ascension of ascending node: | 356.8542° |
| argument of perigee: | 179.6874° |
| revolutions per day: | 11.27575489 |
| mean anomaly at epoch: | 180.4173° |
| orbit number at epoch: | 19176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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