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 56810C 23078AV 24277.46437500 .00025066 00000+0 21006-2 0 2779
2 56810 70.0021 221.1179 0003201 272.0145 214.8935 14.98305375 10
| Epoch (UTC): | 03 October 2024 11:08:42 |
| Eccentricity: | 0.0003201 |
| inclination: | 70.0021° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 221.1179° |
| argument of perigee: | 272.0145° |
| revolutions per day: | 14.98305375 |
| mean anomaly at epoch: | 214.8935° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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