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 25132.67869397 .00000738 00000-0 13016-3 0 9999
2 00029 48.3770 126.8401 0022745 342.7556 17.2583 14.77957521482879
| Epoch (UTC): | 12 May 2025 16:17:19 |
| Eccentricity: | 0.0022745 |
| inclination: | 48.3770° |
| perigee height: | 620 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 126.8401° |
| argument of perigee: | 342.7556° |
| revolutions per day: | 14.77957521 |
| mean anomaly at epoch: | 17.2583° |
| orbit number at epoch: | 48287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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