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 43476U 18047A 23029.63481479 +.00003298 00000-0 +13182-3 0 05
2 43476 88.9910 7.8899 0013572 195.1284 244.7943 15.24987544260886
| Epoch (UTC): | 29 January 2023 15:14:07 |
| Eccentricity: | 0.0013572 |
| inclination: | 88.9910° |
| perigee height: | 481 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 7.8899° |
| argument of perigee: | 195.1284° |
| revolutions per day: | 15.24987544 |
| mean anomaly at epoch: | 244.7943° |
| orbit number at epoch: | 26088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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