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 31793U 07029B 25196.79333337 .00000199 00000-0 12820-3 0 9997
2 31793 70.9774 310.3370 0002242 281.1248 192.9529 14.14791969931867
| Epoch (UTC): | 15 July 2025 19:02:24 |
| Eccentricity: | 0.0002242 |
| inclination: | 70.9774° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 310.3370° |
| argument of perigee: | 281.1248° |
| revolutions per day: | 14.14791969 |
| mean anomaly at epoch: | 192.9529° |
| orbit number at epoch: | 93186 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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