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 26048.58951903 +.00000000 +00000-0 +24172-3 0 00004
2 00011 32.8632 177.7154 1446264 96.3192 280.3535 11.90232594 09
| Epoch (UTC): | 17 February 2026 14:08:54 |
| Eccentricity: | 0.1446264 |
| inclination: | 32.8632° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 177.7154° |
| argument of perigee: | 96.3192° |
| revolutions per day: | 11.90232594 |
| mean anomaly at epoch: | 280.3535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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