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 26932U 26039.15193678 +.00000000 +00000-0 +76831-4 0 00004
2 26932 67.0535 226.3746 0008739 272.4613 87.5488 14.31251965 09
| Epoch (UTC): | 08 February 2026 03:38:47 |
| Eccentricity: | 0.0008739 |
| inclination: | 67.0535° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 226.3746° |
| argument of perigee: | 272.4613° |
| revolutions per day: | 14.31251965 |
| mean anomaly at epoch: | 87.5488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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