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 66795U 26145.42571501 +.00000000 +00000-0 +47213-3 0 00009
2 66795 42.9993 41.1133 0000252 5.5982 354.4872 15.27587086 04
| Epoch (UTC): | 25 May 2026 10:13:01 |
| Eccentricity: | 0.0000252 |
| inclination: | 42.9993° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 41.1133° |
| argument of perigee: | 5.5982° |
| revolutions per day: | 15.27587086 |
| mean anomaly at epoch: | 354.4872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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