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 23335.46650475 .00084939 00000-0 65739-3 0 9994
2 41465 96.9647 204.8378 0004336 354.7510 5.3708 15.71605728426104
| Epoch (UTC): | 01 December 2023 11:11:46 |
| Eccentricity: | 0.0004336 |
| inclination: | 96.9647° |
| perigee height: | 351 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 204.8378° |
| argument of perigee: | 354.7510° |
| revolutions per day: | 15.71605728 |
| mean anomaly at epoch: | 5.3708° |
| orbit number at epoch: | 42610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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