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 09482U 26141.27475681 +.00000000 +00000-0 -11920-4 0 00008
2 09482 81.2594 195.9586 0083993 323.0165 36.5232 14.08002684 03
| Epoch (UTC): | 21 May 2026 06:35:38 |
| Eccentricity: | 0.0083993 |
| inclination: | 81.2594° |
| perigee height: | 805 km |
| apogee height: | 927 km |
| right ascension of ascending node: | 195.9586° |
| argument of perigee: | 323.0165° |
| revolutions per day: | 14.08002684 |
| mean anomaly at epoch: | 36.5232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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