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 is defined by the following mean orbital elements,
1 35935U 26071.21803242 +.00000000 +00000-0 +24744-3 0 00000
2 35935 98.4111 336.5331 0007443 170.1513 189.9834 14.60274470 08
| Epoch (UTC): | 12 March 2026 05:13:58 |
| Eccentricity: | 0.0007443 |
| inclination: | 98.4111° |
| perigee height: | 687 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 336.5331° |
| argument of perigee: | 170.1513° |
| revolutions per day: | 14.60274470 |
| mean anomaly at epoch: | 189.9834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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