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 57405C 23102B 24358.14631944 -.00000053 00000+0 -39484-5 0 3584
2 57405 43.0016 128.2895 0001464 264.6467 123.0686 15.02522658 15
| Epoch (UTC): | 23 December 2024 03:30:42 |
| Eccentricity: | 0.0001464 |
| inclination: | 43.0016° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 128.2895° |
| argument of perigee: | 264.6467° |
| revolutions per day: | 15.02522658 |
| mean anomaly at epoch: | 123.0686° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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