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 25544U 98067A 23159.12120844 .00013971 00000-0 24718-3 0 9998
2 25544 51.6420 13.4809 0005502 61.7246 82.3957 15.50580383400380
| Epoch (UTC): | 08 June 2023 02:54:32 |
| Eccentricity: | 0.0005502 |
| inclination: | 51.6420° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 13.4809° |
| argument of perigee: | 61.7246° |
| revolutions per day: | 15.50580383 |
| mean anomaly at epoch: | 82.3957° |
| orbit number at epoch: | 40038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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