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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 39237U 13045A 25087.12961508 .00000004 00000-0 00000+0 0 9994
2 39237 0.0283 129.4418 0003508 233.2815 294.7098 1.00272348 42415
| Epoch (UTC): | 28 March 2025 03:06:38 |
| Eccentricity: | 0.0003508 |
| inclination: | 0.0283° |
| perigee height: | 35771 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 129.4418° |
| argument of perigee: | 233.2815° |
| revolutions per day: | 1.00272348 |
| mean anomaly at epoch: | 294.7098° |
| orbit number at epoch: | 4241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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