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 66033U 26145.47002220 +.00000000 +00000-0 +17531-3 0 00006
2 66033 89.0020 45.4848 0002102 67.9378 292.1996 13.51005713 01
| Epoch (UTC): | 25 May 2026 11:16:49 |
| Eccentricity: | 0.0002102 |
| inclination: | 89.0020° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4848° |
| argument of perigee: | 67.9378° |
| revolutions per day: | 13.51005713 |
| mean anomaly at epoch: | 292.1996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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