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 37849U 11061A 25189.15856301 .00000038 00000-0 38756-4 0 9998
2 37849 98.7580 128.1119 0000778 175.9131 184.2051 14.19544396709623
| Epoch (UTC): | 08 July 2025 03:48:19 |
| Eccentricity: | 0.0000778 |
| inclination: | 98.7580° |
| perigee height: | 826 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 128.1119° |
| argument of perigee: | 175.9131° |
| revolutions per day: | 14.19544396 |
| mean anomaly at epoch: | 184.2051° |
| orbit number at epoch: | 70962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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