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 24277.15973441 .00002539 00000-0 35515-3 0 9996
2 23343 97.7767 316.5290 0008058 115.9540 292.8389 14.78402102610223
| Epoch (UTC): | 03 October 2024 03:50:01 |
| Eccentricity: | 0.0008058 |
| inclination: | 97.7767° |
| perigee height: | 629 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 316.5290° |
| argument of perigee: | 115.9540° |
| revolutions per day: | 14.78402102 |
| mean anomaly at epoch: | 292.8389° |
| orbit number at epoch: | 61022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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