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 21667U 26067.59396991 +.00000000 +00000-0 +78749-4 0 00006
2 21667 82.9096 156.0409 0020800 14.9812 105.2571 13.75280998 01
| Epoch (UTC): | 08 March 2026 14:15:19 |
| Eccentricity: | 0.0020800 |
| inclination: | 82.9096° |
| perigee height: | 965 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 156.0409° |
| argument of perigee: | 14.9812° |
| revolutions per day: | 13.75280998 |
| mean anomaly at epoch: | 105.2571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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