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 07434U 74071B 24283.62291218 .00001175 00000-0 39895-3 0 9998
2 07434 74.0480 346.1615 0021470 314.8091 45.1316 14.37654874620095
| Epoch (UTC): | 09 October 2024 14:56:59 |
| Eccentricity: | 0.0021470 |
| inclination: | 74.0480° |
| perigee height: | 751 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 346.1615° |
| argument of perigee: | 314.8091° |
| revolutions per day: | 14.37654874 |
| mean anomaly at epoch: | 45.1316° |
| orbit number at epoch: | 62009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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