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 35464U 93036ALJ 24252.09133653 .00110176 00000-0 82237-2 0 9998
2 35464 73.9951 294.8378 0019343 203.2961 183.4909 15.02103270820232
| Epoch (UTC): | 08 September 2024 02:11:31 |
| Eccentricity: | 0.0019343 |
| inclination: | 73.9951° |
| perigee height: | 547 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 294.8378° |
| argument of perigee: | 203.2961° |
| revolutions per day: | 15.02103270 |
| mean anomaly at epoch: | 183.4909° |
| orbit number at epoch: | 82023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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