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 35932U 09051B 25073.66352738 .00003400 00000-0 70386-3 0 9998
2 35932 98.4406 328.2476 0006406 191.2749 168.8308 14.60940455822066
| Epoch (UTC): | 14 March 2025 15:55:28 |
| Eccentricity: | 0.0006406 |
| inclination: | 98.4406° |
| perigee height: | 685 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 328.2476° |
| argument of perigee: | 191.2749° |
| revolutions per day: | 14.60940455 |
| mean anomaly at epoch: | 168.8308° |
| orbit number at epoch: | 82206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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