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 25140.67023131 +.00004260 00000-0 +12732-3 0 02
2 43476 88.9778 252.1921 0011830 185.6682 272.1423 15.34460713389548
| Epoch (UTC): | 20 May 2025 16:05:07 |
| Eccentricity: | 0.0011830 |
| inclination: | 88.9778° |
| perigee height: | 454 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 252.1921° |
| argument of perigee: | 185.6682° |
| revolutions per day: | 15.34460713 |
| mean anomaly at epoch: | 272.1423° |
| orbit number at epoch: | 38954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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