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 33498U 09002G 25162.80020202 .00002731 00000-0 27624-3 0 9995
2 33498 98.1249 92.0244 0008040 319.5088 40.5530 14.91857738883187
| Epoch (UTC): | 11 June 2025 19:12:17 |
| Eccentricity: | 0.0008040 |
| inclination: | 98.1249° |
| perigee height: | 586 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 92.0244° |
| argument of perigee: | 319.5088° |
| revolutions per day: | 14.91857738 |
| mean anomaly at epoch: | 40.5530° |
| orbit number at epoch: | 88318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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