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 08959U 75004AR 24357.81949334 .00001446 00000-0 40632-3 0 9992
2 08959 98.6103 309.9459 0062683 256.6141 102.8057 14.46378965564213
| Epoch (UTC): | 22 December 2024 19:40:04 |
| Eccentricity: | 0.0062683 |
| inclination: | 98.6103° |
| perigee height: | 693 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 309.9459° |
| argument of perigee: | 256.6141° |
| revolutions per day: | 14.46378965 |
| mean anomaly at epoch: | 102.8057° |
| orbit number at epoch: | 56421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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