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 35685U 26103.54658374 +.00000000 +00000-0 +11019-3 0 00009
2 35685 98.1076 220.2401 0049930 18.8771 341.4284 14.92876934 07
| Epoch (UTC): | 13 April 2026 13:07:04 |
| Eccentricity: | 0.0049930 |
| inclination: | 98.1076° |
| perigee height: | 554 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 220.2401° |
| argument of perigee: | 18.8771° |
| revolutions per day: | 14.92876934 |
| mean anomaly at epoch: | 341.4284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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