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 39444U 13066AE 24357.86839105 .00011335 00000-0 95287-3 0 9998
2 39444 97.7436 314.1601 0041621 231.0842 128.6667 14.97772527598292
| Epoch (UTC): | 22 December 2024 20:50:28 |
| Eccentricity: | 0.0041621 |
| inclination: | 97.7436° |
| perigee height: | 545 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 314.1601° |
| argument of perigee: | 231.0842° |
| revolutions per day: | 14.97772527 |
| mean anomaly at epoch: | 128.6667° |
| orbit number at epoch: | 59829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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