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 18417U 26088.17095317 +.00000000 +00000-0 +77108-4 0 00008
2 18417 70.9977 140.3694 0200218 30.6625 38.6117 13.74645494 07
| Epoch (UTC): | 29 March 2026 04:06:10 |
| Eccentricity: | 0.0200218 |
| inclination: | 70.9977° |
| perigee height: | 836 km |
| apogee height: | 1130 km |
| right ascension of ascending node: | 140.3694° |
| argument of perigee: | 30.6625° |
| revolutions per day: | 13.74645494 |
| mean anomaly at epoch: | 38.6117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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