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 23036.25101574 .00000655 00000-0 12667-3 0 9999
2 00029 48.3796 83.6382 0023570 31.3947 328.8367 14.74970918360628
| Epoch (UTC): | 05 February 2023 06:01:27 |
| Eccentricity: | 0.0023570 |
| inclination: | 48.3796° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 83.6382° |
| argument of perigee: | 31.3947° |
| revolutions per day: | 14.74970918 |
| mean anomaly at epoch: | 328.8367° |
| orbit number at epoch: | 36062 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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