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 29709U 07001A 23083.56337273 .00000967 00000-0 12574-3 0 9991
2 29709 98.0096 50.8629 0014216 68.3702 291.9012 14.82929619876018
| Epoch (UTC): | 24 March 2023 13:31:15 |
| Eccentricity: | 0.0014216 |
| inclination: | 98.0096° |
| perigee height: | 610 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 50.8629° |
| argument of perigee: | 68.3702° |
| revolutions per day: | 14.82929619 |
| mean anomaly at epoch: | 291.9012° |
| orbit number at epoch: | 87601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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