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 25188.58404729 .00000282 00000-0 17087-3 0 9992
2 31793 70.9766 327.5924 0001983 279.4624 155.1701 14.14786704930708
| Epoch (UTC): | 07 July 2025 14:01:01 |
| Eccentricity: | 0.0001983 |
| inclination: | 70.9766° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 327.5924° |
| argument of perigee: | 279.4624° |
| revolutions per day: | 14.14786704 |
| mean anomaly at epoch: | 155.1701° |
| orbit number at epoch: | 93070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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