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 26088.19142300 +.00000000 +00000-0 +13735-3 0 00002
2 09482 81.2546 247.3691 0084972 110.4817 250.5500 14.07986196 03
| Epoch (UTC): | 29 March 2026 04:35:38 |
| Eccentricity: | 0.0084972 |
| inclination: | 81.2546° |
| perigee height: | 805 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 247.3691° |
| argument of perigee: | 110.4817° |
| revolutions per day: | 14.07986196 |
| mean anomaly at epoch: | 250.5500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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