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 42794U 17036AF 25138.90338230 .00008995 00000-0 50222-3 0 9995
2 42794 97.5138 117.2101 0096012 82.5020 278.7104 15.09827187431228
| Epoch (UTC): | 18 May 2025 21:40:52 |
| Eccentricity: | 0.0096012 |
| inclination: | 97.5138° |
| perigee height: | 470 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 117.2101° |
| argument of perigee: | 82.5020° |
| revolutions per day: | 15.09827187 |
| mean anomaly at epoch: | 278.7104° |
| orbit number at epoch: | 43122 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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