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 14659U 84005A 23341.33334508 -.00000236 00000-0 00000-0 0 9996
2 14659 12.4345 330.9619 0019880 198.7736 349.5400 0.99052430109179
| Epoch (UTC): | 07 December 2023 08:00:01 |
| Eccentricity: | 0.0019880 |
| inclination: | 12.4345° |
| perigee height: | 36047 km |
| apogee height: | 36216 km |
| right ascension of ascending node: | 330.9619° |
| argument of perigee: | 198.7736° |
| revolutions per day: | 0.99052430 |
| mean anomaly at epoch: | 349.5400° |
| orbit number at epoch: | 10917 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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