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 41465U 16026B 23266.07070141 .00045024 00000-0 48255-3 0 9996
2 41465 96.9797 135.9235 0004719 204.7614 155.3420 15.63696333415232
| Epoch (UTC): | 23 September 2023 01:41:48 |
| Eccentricity: | 0.0004719 |
| inclination: | 96.9797° |
| perigee height: | 374 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 135.9235° |
| argument of perigee: | 204.7614° |
| revolutions per day: | 15.63696333 |
| mean anomaly at epoch: | 155.3420° |
| orbit number at epoch: | 41523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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