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 35684U 26145.46492903 +.00000000 +00000-0 +85353-4 0 00002
2 35684 98.1414 220.3329 0044061 36.8975 323.5256 14.83841705 06
| Epoch (UTC): | 25 May 2026 11:09:29 |
| Eccentricity: | 0.0044061 |
| inclination: | 98.1414° |
| perigee height: | 586 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 220.3329° |
| argument of perigee: | 36.8975° |
| revolutions per day: | 14.83841705 |
| mean anomaly at epoch: | 323.5256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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