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 23335.97586471 .00082128 00000-0 63332-3 0 9999
2 41465 96.9645 205.3467 0004309 353.6451 6.4758 15.71702149426189
| Epoch (UTC): | 01 December 2023 23:25:14 |
| Eccentricity: | 0.0004309 |
| inclination: | 96.9645° |
| perigee height: | 351 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 205.3467° |
| argument of perigee: | 353.6451° |
| revolutions per day: | 15.71702149 |
| mean anomaly at epoch: | 6.4758° |
| orbit number at epoch: | 42618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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