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 09662U 26088.18644338 +.00000000 +00000-0 +83403-4 0 00009
2 09662 81.2726 249.1503 0052871 122.5159 238.1132 14.01300259 08
| Epoch (UTC): | 29 March 2026 04:28:28 |
| Eccentricity: | 0.0052871 |
| inclination: | 81.2726° |
| perigee height: | 851 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 249.1503° |
| argument of perigee: | 122.5159° |
| revolutions per day: | 14.01300259 |
| mean anomaly at epoch: | 238.1132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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