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 29919U 99025HR 24358.05191743 .00000481 00000-0 42834-3 0 9994
2 29919 98.4501 180.8612 0137412 234.4273 245.6036 13.84871384906376
| Epoch (UTC): | 23 December 2024 01:14:45 |
| Eccentricity: | 0.0137412 |
| inclination: | 98.4501° |
| perigee height: | 846 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 180.8612° |
| argument of perigee: | 234.4273° |
| revolutions per day: | 13.84871384 |
| mean anomaly at epoch: | 245.6036° |
| orbit number at epoch: | 90637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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