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 10664U 26053.80402420 +.00000000 +00000-0 +42409-4 0 00009
2 10664 65.3704 101.2281 1897342 42.1072 331.0983 10.75886896 04
| Epoch (UTC): | 22 February 2026 19:17:47 |
| Eccentricity: | 0.1897342 |
| inclination: | 65.3704° |
| perigee height: | 645 km |
| apogee height: | 3934 km |
| right ascension of ascending node: | 101.2281° |
| argument of perigee: | 42.1072° |
| revolutions per day: | 10.75886896 |
| mean anomaly at epoch: | 331.0983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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