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 38248U 12017A 24358.02365582 .00024735 00000-0 78762-3 0 9993
2 38248 97.5104 17.0623 0001163 0.1596 359.9646 15.32558602698433
| Epoch (UTC): | 23 December 2024 00:34:03 |
| Eccentricity: | 0.0001163 |
| inclination: | 97.5104° |
| perigee height: | 467 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 17.0623° |
| argument of perigee: | 0.1596° |
| revolutions per day: | 15.32558602 |
| mean anomaly at epoch: | 359.9646° |
| orbit number at epoch: | 69843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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