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 02091U 26153.29599647 +.00000000 +00000-0 +93153-4 0 00008
2 02091 101.2341 62.8960 0038388 287.0980 188.1542 12.69430822 07
| Epoch (UTC): | 02 June 2026 07:06:14 |
| Eccentricity: | 0.0038388 |
| inclination: | 101.2341° |
| perigee height: | 1354 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 62.8960° |
| argument of perigee: | 287.0980° |
| revolutions per day: | 12.69430822 |
| mean anomaly at epoch: | 188.1542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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