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 34054U 93036JR 24279.56376339 .00108764 00000-0 11257-1 0 9996
2 34054 74.0264 28.8808 0014734 252.3746 117.5097 14.89368237830049
| Epoch (UTC): | 05 October 2024 13:31:49 |
| Eccentricity: | 0.0014734 |
| inclination: | 74.0264° |
| perigee height: | 589 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 28.8808° |
| argument of perigee: | 252.3746° |
| revolutions per day: | 14.89368237 |
| mean anomaly at epoch: | 117.5097° |
| orbit number at epoch: | 83004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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