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 09988U 26110.10429119 +.00000000 +00000-0 +13832-2 0 00003
2 09988 103.0356 154.8466 0212744 17.2931 343.5322 13.95695147 03
| Epoch (UTC): | 20 April 2026 02:30:10 |
| Eccentricity: | 0.0212744 |
| inclination: | 103.0356° |
| perigee height: | 754 km |
| apogee height: | 1064 km |
| right ascension of ascending node: | 154.8466° |
| argument of perigee: | 17.2931° |
| revolutions per day: | 13.95695147 |
| mean anomaly at epoch: | 343.5322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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