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 00011U 26038.85487330 +.00000000 +00000-0 +33329-3 0 00005
2 00011 32.8626 214.5503 1446526 40.9345 329.1281 11.90222190 07
| Epoch (UTC): | 07 February 2026 20:31:01 |
| Eccentricity: | 0.1446526 |
| inclination: | 32.8626° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 214.5503° |
| argument of perigee: | 40.9345° |
| revolutions per day: | 11.90222190 |
| mean anomaly at epoch: | 329.1281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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