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 40920U 15050A 25109.18436002 .00000033 00000-0 16697-3 0 9995
2 40920 82.4952 343.6330 0008918 189.5385 170.5526 12.42909363434213
| Epoch (UTC): | 19 April 2025 04:25:28 |
| Eccentricity: | 0.0008918 |
| inclination: | 82.4952° |
| perigee height: | 1487 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 343.6330° |
| argument of perigee: | 189.5385° |
| revolutions per day: | 12.42909363 |
| mean anomaly at epoch: | 170.5526° |
| orbit number at epoch: | 43421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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