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 26037.62276947 +.00000000 +00000-0 +00000-0 0 00004
2 26390 59.3801 162.5323 0001176 42.9178 136.0594 1.57877288 07
| Epoch (UTC): | 06 February 2026 14:56:47 |
| Eccentricity: | 0.0001176 |
| inclination: | 59.3801° |
| perigee height: | 24773 km |
| apogee height: | 24780 km |
| right ascension of ascending node: | 162.5323° |
| argument of perigee: | 42.9178° |
| revolutions per day: | 1.57877288 |
| mean anomaly at epoch: | 136.0594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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