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 26931U 26069.46637528 +.00000000 +00000-0 +10460-3 0 00002
2 26931 67.0505 139.6043 0007018 265.1620 94.8681 14.31912733 00
| Epoch (UTC): | 10 March 2026 11:11:34 |
| Eccentricity: | 0.0007018 |
| inclination: | 67.0505° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 139.6043° |
| argument of perigee: | 265.1620° |
| revolutions per day: | 14.31912733 |
| mean anomaly at epoch: | 94.8681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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