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 23705U 95058B 24279.14686109 .00000455 00000-0 25744-3 0 9992
2 23705 71.0224 193.0420 0013295 203.0314 157.0214 14.15382603494490
| Epoch (UTC): | 05 October 2024 03:31:28 |
| Eccentricity: | 0.0013295 |
| inclination: | 71.0224° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 193.0420° |
| argument of perigee: | 203.0314° |
| revolutions per day: | 14.15382603 |
| mean anomaly at epoch: | 157.0214° |
| orbit number at epoch: | 49449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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