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 36834U 10038A 24277.21423792 .00003833 00000-0 47498-3 0 9990
2 36834 97.9455 293.7545 0001502 84.4897 343.6566 14.83278169765019
| Epoch (UTC): | 03 October 2024 05:08:30 |
| Eccentricity: | 0.0001502 |
| inclination: | 97.9455° |
| perigee height: | 618 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 293.7545° |
| argument of perigee: | 84.4897° |
| revolutions per day: | 14.83278169 |
| mean anomaly at epoch: | 343.6566° |
| orbit number at epoch: | 76501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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