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 34136U 93036LH 24280.68456083 .00013944 00000-0 19357-2 0 9992
2 34136 74.0216 171.6629 0093348 44.2840 340.0657 14.74921709836286
| Epoch (UTC): | 06 October 2024 16:25:46 |
| Eccentricity: | 0.0093348 |
| inclination: | 74.0216° |
| perigee height: | 580 km |
| apogee height: | 711 km |
| right ascension of ascending node: | 171.6629° |
| argument of perigee: | 44.2840° |
| revolutions per day: | 14.74921709 |
| mean anomaly at epoch: | 340.0657° |
| orbit number at epoch: | 83628 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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