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 28737U 05024A 24358.00303687 .00012630 00000-0 76688-3 0 9997
2 28737 97.7666 5.3267 0021847 96.7602 263.6114 15.10446354 66025
| Epoch (UTC): | 23 December 2024 00:04:22 |
| Eccentricity: | 0.0021847 |
| inclination: | 97.7666° |
| perigee height: | 520 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 5.3267° |
| argument of perigee: | 96.7602° |
| revolutions per day: | 15.10446354 |
| mean anomaly at epoch: | 263.6114° |
| orbit number at epoch: | 6602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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