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 07493U 74083B 23340.52906037 .00000096 00000-0 48801-4 0 9999
2 07493 81.1613 8.4948 0079412 275.0873 84.1236 14.07742677520953
| Epoch (UTC): | 06 December 2023 12:41:50 |
| Eccentricity: | 0.0079412 |
| inclination: | 81.1613° |
| perigee height: | 809 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 8.4948° |
| argument of perigee: | 275.0873° |
| revolutions per day: | 14.07742677 |
| mean anomaly at epoch: | 84.1236° |
| orbit number at epoch: | 52095 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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