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 21688U 26150.53325272 +.00000000 +00000-0 +45061-8 0 00005
2 21688 99.4104 158.0399 0024976 52.9326 118.5014 13.97868954 04
| Epoch (UTC): | 30 May 2026 12:47:53 |
| Eccentricity: | 0.0024976 |
| inclination: | 99.4104° |
| perigee height: | 883 km |
| apogee height: | 919 km |
| right ascension of ascending node: | 158.0399° |
| argument of perigee: | 52.9326° |
| revolutions per day: | 13.97868954 |
| mean anomaly at epoch: | 118.5014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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