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 57072U 23088AA 25321.47197719 .00008209 00000-0 61883-3 0 9998
2 57072 43.0048 344.7135 0001380 272.7149 87.3535 15.02731580132653
| Epoch (UTC): | 17 November 2025 11:19:38 |
| Eccentricity: | 0.0001380 |
| inclination: | 43.0048° |
| perigee height: | 557 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 344.7135° |
| argument of perigee: | 272.7149° |
| revolutions per day: | 15.02731580 |
| mean anomaly at epoch: | 87.3535° |
| orbit number at epoch: | 13265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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