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 25167.13449508 .00000749 00000-0 16773-3 0 9992
2 35935 98.4324 63.3702 0006484 299.9244 60.1310 14.59560982835353
| Epoch (UTC): | 16 June 2025 03:13:40 |
| Eccentricity: | 0.0006484 |
| inclination: | 98.4324° |
| perigee height: | 690 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 63.3702° |
| argument of perigee: | 299.9244° |
| revolutions per day: | 14.59560982 |
| mean anomaly at epoch: | 60.1310° |
| orbit number at epoch: | 83535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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