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 38725U 99025ETS 24356.26856550 .00012459 00000-0 43547-2 0 9993
2 38725 98.8567 103.6364 0039448 231.0730 128.6935 14.34890330682259
| Epoch (UTC): | 21 December 2024 06:26:44 |
| Eccentricity: | 0.0039448 |
| inclination: | 98.8567° |
| perigee height: | 747 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 103.6364° |
| argument of perigee: | 231.0730° |
| revolutions per day: | 14.34890330 |
| mean anomaly at epoch: | 128.6935° |
| orbit number at epoch: | 68225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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