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 56120C 23046AD 24252.45534722 .00011369 00000+0 83895-3 0 2523
2 56120 43.0016 239.9678 0001322 265.7996 259.4489 15.02520301 17
| Epoch (UTC): | 08 September 2024 10:55:42 |
| Eccentricity: | 0.0001322 |
| inclination: | 43.0016° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 239.9678° |
| argument of perigee: | 265.7996° |
| revolutions per day: | 15.02520301 |
| mean anomaly at epoch: | 259.4489° |
| 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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