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 29507U 06046C 25191.60199381 .00002778 00000-0 15442-3 0 9997
2 29507 97.5937 232.1553 0036018 27.0964 333.2137 15.13991417 23381
| Epoch (UTC): | 10 July 2025 14:26:52 |
| Eccentricity: | 0.0036018 |
| inclination: | 97.5937° |
| perigee height: | 499 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 232.1553° |
| argument of perigee: | 27.0964° |
| revolutions per day: | 15.13991417 |
| mean anomaly at epoch: | 333.2137° |
| orbit number at epoch: | 2338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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