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 00172U 61015AY 25316.25373224 .00000404 00000-0 60433-3 0 9995
2 00172 67.0673 304.7912 0137729 220.7700 138.2995 13.59090652175633
| Epoch (UTC): | 12 November 2025 06:05:22 |
| Eccentricity: | 0.0137729 |
| inclination: | 67.0673° |
| perigee height: | 937 km |
| apogee height: | 1141 km |
| right ascension of ascending node: | 304.7912° |
| argument of perigee: | 220.7700° |
| revolutions per day: | 13.59090652 |
| mean anomaly at epoch: | 138.2995° |
| orbit number at epoch: | 17563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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