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 25634U 99008A 23150.42917666 .00000065 00000-0 50155-4 0 9999
2 25634 98.3937 151.6030 0010917 37.8656 322.3287 14.19526696256267
| Epoch (UTC): | 30 May 2023 10:18:00 |
| Eccentricity: | 0.0010917 |
| inclination: | 98.3937° |
| perigee height: | 819 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 151.6030° |
| argument of perigee: | 37.8656° |
| revolutions per day: | 14.19526696 |
| mean anomaly at epoch: | 322.3287° |
| orbit number at epoch: | 25626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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