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 00029U 60002B 25339.05424223 .00001436 00000-0 22337-3 0 9997
2 00029 48.3775 227.0239 0022181 153.5036 206.7016 14.78396533513403
| Epoch (UTC): | 05 December 2025 01:18:06 |
| Eccentricity: | 0.0022181 |
| inclination: | 48.3775° |
| perigee height: | 619 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 227.0239° |
| argument of perigee: | 153.5036° |
| revolutions per day: | 14.78396533 |
| mean anomaly at epoch: | 206.7016° |
| orbit number at epoch: | 51340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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