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 35683U 26145.65130117 +.00000000 +00000-0 +68479-4 0 00008
2 35683 97.8802 281.1735 0001485 76.6114 283.5261 14.75984070 03
| Epoch (UTC): | 25 May 2026 15:37:52 |
| Eccentricity: | 0.0001485 |
| inclination: | 97.8802° |
| perigee height: | 641 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 281.1735° |
| argument of perigee: | 76.6114° |
| revolutions per day: | 14.75984070 |
| mean anomaly at epoch: | 283.5261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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