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 40907U 15049J 24320.92351917 .16701952 27880-5 21132-3 0 9990
2 40907 97.4221 349.6759 0008313 198.6926 161.4075 16.49393757508467
| Epoch (UTC): | 15 November 2024 22:09:52 |
| Eccentricity: | 0.0008313 |
| inclination: | 97.4221° |
| perigee height: | 135 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 349.6759° |
| argument of perigee: | 198.6926° |
| revolutions per day: | 16.49393757 |
| mean anomaly at epoch: | 161.4075° |
| orbit number at epoch: | 50846 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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