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 31123U 07012G 25196.91622797 .00000011 00000-0 19605-4 0 9993
2 31123 98.0563 70.3434 0308741 303.9628 63.3947 14.13403990940715
| Epoch (UTC): | 15 July 2025 21:59:22 |
| Eccentricity: | 0.0308741 |
| inclination: | 98.0563° |
| perigee height: | 624 km |
| apogee height: | 1071 km |
| right ascension of ascending node: | 70.3434° |
| argument of perigee: | 303.9628° |
| revolutions per day: | 14.13403990 |
| mean anomaly at epoch: | 63.3947° |
| orbit number at epoch: | 94071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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