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 35935U 09051E 24282.41664602 .00015998 00000-0 34542-2 0 9999
2 35935 98.4545 168.4158 0007879 0.0888 0.0310 14.58392127798763
| Epoch (UTC): | 08 October 2024 09:59:58 |
| Eccentricity: | 0.0007879 |
| inclination: | 98.4545° |
| perigee height: | 693 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 168.4158° |
| argument of perigee: | 0.0888° |
| revolutions per day: | 14.58392127 |
| mean anomaly at epoch: | 0.0310° |
| orbit number at epoch: | 79876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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