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 35946U 26145.61802876 +.00000000 +00000-0 +47499-4 0 00003
2 35946 98.4681 219.3800 0003139 292.8744 67.2112 14.37937112 07
| Epoch (UTC): | 25 May 2026 14:49:57 |
| Eccentricity: | 0.0003139 |
| inclination: | 98.4681° |
| perigee height: | 763 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 219.3800° |
| argument of perigee: | 292.8744° |
| revolutions per day: | 14.37937112 |
| mean anomaly at epoch: | 67.2112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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