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 35935U 09051E 25080.26998905 .00002882 00000-0 62019-3 0 9994
2 35935 98.4411 335.0813 0007087 193.3349 166.7663 14.59278863822652
| Epoch (UTC): | 21 March 2025 06:28:47 |
| Eccentricity: | 0.0007087 |
| inclination: | 98.4411° |
| perigee height: | 690 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 335.0813° |
| argument of perigee: | 193.3349° |
| revolutions per day: | 14.59278863 |
| mean anomaly at epoch: | 166.7663° |
| orbit number at epoch: | 82265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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