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 00059U 60013B 24276.85110244 .00000364 00000-0 36579-3 0 9996
2 00059 28.2476 81.2024 0188889 131.0037 230.7007 13.53094636158811
| Epoch (UTC): | 02 October 2024 20:25:35 |
| Eccentricity: | 0.0188889 |
| inclination: | 28.2476° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 81.2024° |
| argument of perigee: | 131.0037° |
| revolutions per day: | 13.53094636 |
| mean anomaly at epoch: | 230.7007° |
| orbit number at epoch: | 15881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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