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 26390U 26084.17709476 +.00000000 +00000-0 +00000-0 0 00004
2 26390 59.3779 161.5999 0001818 308.4252 50.4730 1.57877157 01
| Epoch (UTC): | 25 March 2026 04:15:00 |
| Eccentricity: | 0.0001818 |
| inclination: | 59.3779° |
| perigee height: | 24771 km |
| apogee height: | 24782 km |
| right ascension of ascending node: | 161.5999° |
| argument of perigee: | 308.4252° |
| revolutions per day: | 1.57877157 |
| mean anomaly at epoch: | 50.4730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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