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 4438U 69082EK 24358.38587202 .00007288 00000-0 14179-2 0 9990
2 4438 70.0991 85.3852 0051709 235.9398 123.6829 14.62590241896041
| Epoch (UTC): | 23 December 2024 09:15:39 |
| Eccentricity: | 0.0051709 |
| inclination: | 70.0991° |
| perigee height: | 648 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 85.3852° |
| argument of perigee: | 235.9398° |
| revolutions per day: | 14.62590241 |
| mean anomaly at epoch: | 123.6829° |
| orbit number at epoch: | 89604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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