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 66045U 26145.22316772 +.00000000 +00000-0 +19454-3 0 00008
2 66045 89.0026 45.5150 0002156 68.4415 291.6966 13.51007295 02
| Epoch (UTC): | 25 May 2026 05:21:21 |
| Eccentricity: | 0.0002156 |
| inclination: | 89.0026° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.5150° |
| argument of perigee: | 68.4415° |
| revolutions per day: | 13.51007295 |
| mean anomaly at epoch: | 291.6966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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