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 66048U 26145.23140726 +.00000000 +00000-0 +19780-3 0 00008
2 66048 89.0013 45.4754 0001921 81.8868 278.2501 13.51006552 01
| Epoch (UTC): | 25 May 2026 05:33:13 |
| Eccentricity: | 0.0001921 |
| inclination: | 89.0013° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4754° |
| argument of perigee: | 81.8868° |
| revolutions per day: | 13.51006552 |
| mean anomaly at epoch: | 278.2501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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