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 06236U 72082B 25012.68761441 -.00000022 00000-0 15521-3 0 9995
2 06236 102.0211 25.3362 0004443 64.2913 55.2000 12.53197683389767
| Epoch (UTC): | 12 January 2025 16:30:09 |
| Eccentricity: | 0.0004443 |
| inclination: | 102.0211° |
| perigee height: | 1447 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 25.3362° |
| argument of perigee: | 64.2913° |
| revolutions per day: | 12.53197683 |
| mean anomaly at epoch: | 55.2000° |
| orbit number at epoch: | 38976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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