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 26048.75732987 +.00000000 +00000-0 +24127-3 0 00002
2 00011 32.8632 177.0805 1446263 97.2737 279.3966 11.90232767 07
| Epoch (UTC): | 17 February 2026 18:10:33 |
| Eccentricity: | 0.1446263 |
| inclination: | 32.8632° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 177.0805° |
| argument of perigee: | 97.2737° |
| revolutions per day: | 11.90232767 |
| mean anomaly at epoch: | 279.3966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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