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 60235U 24128A 24288.55150384 .00005268 00000-0 48038-3 0 9995
2 60235 61.9965 188.2174 0022890 330.2453 29.7331 14.96123244 14462
| Epoch (UTC): | 14 October 2024 13:14:09 |
| Eccentricity: | 0.0022890 |
| inclination: | 61.9965° |
| perigee height: | 563 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 188.2174° |
| argument of perigee: | 330.2453° |
| revolutions per day: | 14.96123244 |
| mean anomaly at epoch: | 29.7331° |
| orbit number at epoch: | 1446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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