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 08756U 74071C 23340.30840348 .00008290 00000-0 97316-3 0 9995
2 08756 74.0508 297.1755 0005251 244.6064 115.4572 14.85055775752148
| Epoch (UTC): | 06 December 2023 07:24:06 |
| Eccentricity: | 0.0005251 |
| inclination: | 74.0508° |
| perigee height: | 610 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 297.1755° |
| argument of perigee: | 244.6064° |
| revolutions per day: | 14.85055775 |
| mean anomaly at epoch: | 115.4572° |
| orbit number at epoch: | 75214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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