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 35123U 99025DLB 23337.86776939 .00002119 00000-0 99715-3 0 9999
2 35123 99.0658 125.4853 0053249 31.2269 329.2052 14.20337850505553
| Epoch (UTC): | 03 December 2023 20:49:35 |
| Eccentricity: | 0.0053249 |
| inclination: | 99.0658° |
| perigee height: | 786 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 125.4853° |
| argument of perigee: | 31.2269° |
| revolutions per day: | 14.20337850 |
| mean anomaly at epoch: | 329.2052° |
| orbit number at epoch: | 50555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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