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 40921U 15050B 25312.87083731 .00000047 00000-0 26992-3 0 9999
2 40921 82.4900 215.3910 0013944 140.2638 219.9466 12.42904020459477
| Epoch (UTC): | 08 November 2025 20:54:00 |
| Eccentricity: | 0.0013944 |
| inclination: | 82.4900° |
| perigee height: | 1483 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 215.3910° |
| argument of perigee: | 140.2638° |
| revolutions per day: | 12.42904020 |
| mean anomaly at epoch: | 219.9466° |
| orbit number at epoch: | 45947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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