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 34486U 97051GB 25322.22102177 .00028118 00000-0 26058-2 0 9996
2 34486 86.3967 23.3248 0011536 194.9758 227.4041 14.94297043886204
| Epoch (UTC): | 18 November 2025 05:18:16 |
| Eccentricity: | 0.0011536 |
| inclination: | 86.3967° |
| perigee height: | 576 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 23.3248° |
| argument of perigee: | 194.9758° |
| revolutions per day: | 14.94297043 |
| mean anomaly at epoch: | 227.4041° |
| orbit number at epoch: | 88620 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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