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 23157.06009020 .00014500 00000-0 25676-3 0 9994
2 25544 51.6427 23.6999 0005744 51.6360 99.7596 15.50520310400063
| Epoch (UTC): | 06 June 2023 01:26:31 |
| Eccentricity: | 0.0005744 |
| inclination: | 51.6427° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 23.6999° |
| argument of perigee: | 51.6360° |
| revolutions per day: | 15.50520310 |
| mean anomaly at epoch: | 99.7596° |
| orbit number at epoch: | 40006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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