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 23277.89490741 .00019371 00000-0 34902-3 0 9995
2 25544 51.6403 145.1350 0005654 71.4221 108.5872 15.49787428418804
| Epoch (UTC): | 04 October 2023 21:28:40 |
| Eccentricity: | 0.0005654 |
| inclination: | 51.6403° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 145.1350° |
| argument of perigee: | 71.4221° |
| revolutions per day: | 15.49787428 |
| mean anomaly at epoch: | 108.5872° |
| orbit number at epoch: | 41880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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