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 60740C 24152W 25136.75465278 .00001559 00000+0 52541-4 0 1365
2 60740 53.1583 207.8146 0001233 89.1723 19.0735 15.30191544 10
| Epoch (UTC): | 16 May 2025 18:06:42 |
| Eccentricity: | 0.0001233 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.8146° |
| argument of perigee: | 89.1723° |
| revolutions per day: | 15.30191544 |
| mean anomaly at epoch: | 19.0735° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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