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 15482U 85006A 23334.83430825 .00000543 00000-0 20619-3 0 9990
2 15482 74.0425 92.7942 0014913 207.3195 269.9997 14.33364743 31353
| Epoch (UTC): | 30 November 2023 20:01:24 |
| Eccentricity: | 0.0014913 |
| inclination: | 74.0425° |
| perigee height: | 770 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 92.7942° |
| argument of perigee: | 207.3195° |
| revolutions per day: | 14.33364743 |
| mean anomaly at epoch: | 269.9997° |
| orbit number at epoch: | 3135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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