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 21666U 26106.68170006 +.00000000 +00000-0 +53407-4 0 00000
2 21666 82.9071 155.0705 0025617 26.8574 92.3729 13.73534568 03
| Epoch (UTC): | 16 April 2026 16:21:38 |
| Eccentricity: | 0.0025617 |
| inclination: | 82.9071° |
| perigee height: | 968 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 155.0705° |
| argument of perigee: | 26.8574° |
| revolutions per day: | 13.73534568 |
| mean anomaly at epoch: | 92.3729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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