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 31279U 99025BNM 25190.79144136 .00000619 00000-0 27099-3 0 9995
2 31279 98.5188 203.3448 0072517 274.7682 84.5220 14.25806716950066
| Epoch (UTC): | 09 July 2025 18:59:40 |
| Eccentricity: | 0.0072517 |
| inclination: | 98.5188° |
| perigee height: | 753 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 203.3448° |
| argument of perigee: | 274.7682° |
| revolutions per day: | 14.25806716 |
| mean anomaly at epoch: | 84.5220° |
| orbit number at epoch: | 95006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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