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 20740U 90070F 25341.09298368 .00000039 00000-0 14844-3 0 9995
2 20740 82.5749 31.0545 0020500 94.9113 291.1391 12.66135768632723
| Epoch (UTC): | 07 December 2025 02:13:53 |
| Eccentricity: | 0.0020500 |
| inclination: | 82.5749° |
| perigee height: | 1382 km |
| apogee height: | 1413 km |
| right ascension of ascending node: | 31.0545° |
| argument of perigee: | 94.9113° |
| revolutions per day: | 12.66135768 |
| mean anomaly at epoch: | 291.1391° |
| orbit number at epoch: | 63272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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