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 is defined by the following mean orbital elements,
1 47097U 20087A 24053.28652788 -.00013071 00000-0 00000+0 0 9996
2 47097 30.7677 10.7618 3781869 349.8514 126.8236 0.04182964 639
| Epoch (UTC): | 22 February 2024 06:52:36 |
| Eccentricity: | 0.3781869 |
| inclination: | 30.7677° |
| perigee height: | 211593 km |
| apogee height: | 476734 km |
| right ascension of ascending node: | 10.7618° |
| argument of perigee: | 349.8514° |
| revolutions per day: | 0.04182964 |
| mean anomaly at epoch: | 126.8236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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