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 20666U 90055D 25348.89622546 .00001839 00000-0 15012-3 0 9996
2 20666 62.7820 182.0884 0012935 310.5499 49.4473 15.03085436925449
| Epoch (UTC): | 14 December 2025 21:30:33 |
| Eccentricity: | 0.0012935 |
| inclination: | 62.7820° |
| perigee height: | 548 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 182.0884° |
| argument of perigee: | 310.5499° |
| revolutions per day: | 15.03085436 |
| mean anomaly at epoch: | 49.4473° |
| orbit number at epoch: | 92544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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