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 23343U 94074B 24282.58824887 .00003523 00000-0 48976-3 0 9997
2 23343 97.7754 321.7726 0008159 101.7021 21.5881 14.78431610610815
| Epoch (UTC): | 08 October 2024 14:07:04 |
| Eccentricity: | 0.0008159 |
| inclination: | 97.7754° |
| perigee height: | 628 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 321.7726° |
| argument of perigee: | 101.7021° |
| revolutions per day: | 14.78431610 |
| mean anomaly at epoch: | 21.5881° |
| orbit number at epoch: | 61081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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