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 00029U 60002B 23088.68095231 .00001757 00000-0 28674-3 0 9994
2 00029 48.3791 195.9281 0024451 257.8899 101.9273 14.75163545368364
| Epoch (UTC): | 29 March 2023 16:20:34 |
| Eccentricity: | 0.0024451 |
| inclination: | 48.3791° |
| perigee height: | 627 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 195.9281° |
| argument of perigee: | 257.8899° |
| revolutions per day: | 14.75163545 |
| mean anomaly at epoch: | 101.9273° |
| orbit number at epoch: | 36836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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