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 29092U 06015A 23028.54498996 .00000965 00000-0 12301-3 0 9993
2 29092 97.8538 58.1030 0001419 90.4154 269.7223 14.83756707906317
| Epoch (UTC): | 28 January 2023 13:04:47 |
| Eccentricity: | 0.0001419 |
| inclination: | 97.8538° |
| perigee height: | 616 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 58.1030° |
| argument of perigee: | 90.4154° |
| revolutions per day: | 14.83756707 |
| mean anomaly at epoch: | 269.7223° |
| orbit number at epoch: | 90631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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