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 25197.54624793 .00000042 00000-0 41002-4 0 9991
2 37849 98.7580 136.4078 0001260 156.5976 203.5257 14.19545973710816
| Epoch (UTC): | 16 July 2025 13:06:35 |
| Eccentricity: | 0.0001260 |
| inclination: | 98.7580° |
| perigee height: | 826 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 136.4078° |
| argument of perigee: | 156.5976° |
| revolutions per day: | 14.19545973 |
| mean anomaly at epoch: | 203.5257° |
| orbit number at epoch: | 71081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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