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 26076.16683028 +.00000000 +00000-0 +40262-4 0 00008
2 21667 82.9082 149.6581 0020236 351.1172 69.5559 13.75281738 04
| Epoch (UTC): | 17 March 2026 04:00:14 |
| Eccentricity: | 0.0020236 |
| inclination: | 82.9082° |
| perigee height: | 966 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 149.6581° |
| argument of perigee: | 351.1172° |
| revolutions per day: | 13.75281738 |
| mean anomaly at epoch: | 69.5559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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