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 43615U 18070C 23040.90006581 .03225936 16756-6 13613-2 0 9990
2 43615 92.9864 200.7271 0007018 283.5819 76.4699 16.22968473248238
| Epoch (UTC): | 09 February 2023 21:36:05 |
| Eccentricity: | 0.0007018 |
| inclination: | 92.9864° |
| perigee height: | 207 km |
| apogee height: | 216 km |
| right ascension of ascending node: | 200.7271° |
| argument of perigee: | 283.5819° |
| revolutions per day: | 16.22968473 |
| mean anomaly at epoch: | 76.4699° |
| orbit number at epoch: | 24823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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