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 40074U 14037F 24340.59472283 .00017346 00000-0 14117-2 0 9990
2 40074 98.3581 281.8120 0001950 137.8754 222.2617 14.99609746564410
| Epoch (UTC): | 05 December 2024 14:16:24 |
| Eccentricity: | 0.0001950 |
| inclination: | 98.3581° |
| perigee height: | 567 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 281.8120° |
| argument of perigee: | 137.8754° |
| revolutions per day: | 14.99609746 |
| mean anomaly at epoch: | 222.2617° |
| orbit number at epoch: | 56441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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