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 26053.62912117 +.00000000 +00000-0 +52767-4 0 00000
2 21666 82.9083 194.4474 0025454 168.4074 208.4220 13.73529832 07
| Epoch (UTC): | 22 February 2026 15:05:56 |
| Eccentricity: | 0.0025454 |
| inclination: | 82.9083° |
| perigee height: | 968 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 194.4474° |
| argument of perigee: | 168.4074° |
| revolutions per day: | 13.73529832 |
| mean anomaly at epoch: | 208.4220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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