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 23851U 96024A 25114.80474929 -.00000075 00000-0 -22244-4 0 9998
2 23851 99.0042 53.7860 0006755 313.6947 46.3657 13.98332117479874
| Epoch (UTC): | 24 April 2025 19:18:50 |
| Eccentricity: | 0.0006755 |
| inclination: | 99.0042° |
| perigee height: | 894 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 53.7860° |
| argument of perigee: | 313.6947° |
| revolutions per day: | 13.98332117 |
| mean anomaly at epoch: | 46.3657° |
| orbit number at epoch: | 47987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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