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 35933U 09051C 25073.60439681 .00002825 00000-0 59336-3 0 9998
2 35933 98.4336 328.6933 0004603 202.7665 157.3331 14.60413055822074
| Epoch (UTC): | 14 March 2025 14:30:19 |
| Eccentricity: | 0.0004603 |
| inclination: | 98.4336° |
| perigee height: | 688 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 328.6933° |
| argument of perigee: | 202.7665° |
| revolutions per day: | 14.60413055 |
| mean anomaly at epoch: | 157.3331° |
| orbit number at epoch: | 82207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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