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 29U 60002B 23087.80040396 .00001613 00000-0 26573-3 0 9996
2 29 48.3791 200.0888 0024442 254.1804 105.6413 14.75159292368340
| Epoch (UTC): | 28 March 2023 19:12:34 |
| Eccentricity: | 0.0024442 |
| inclination: | 48.3791° |
| perigee height: | 627 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 200.0888° |
| argument of perigee: | 254.1804° |
| revolutions per day: | 14.75159292 |
| mean anomaly at epoch: | 105.6413° |
| orbit number at epoch: | 36834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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