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 29U 60002B 25317.08832391 .00001838 00000-0 27807-3 0 9998
2 29 48.3788 331.3487 0021937 56.8437 303.4577 14.78336780510153
| Epoch (UTC): | 13 November 2025 02:07:11 |
| Eccentricity: | 0.0021937 |
| inclination: | 48.3788° |
| perigee height: | 619 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 331.3487° |
| argument of perigee: | 56.8437° |
| revolutions per day: | 14.78336780 |
| mean anomaly at epoch: | 303.4577° |
| orbit number at epoch: | 51015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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