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 66070U 26145.54256160 +.00000000 +00000-0 -37773-3 0 00000
2 66070 53.1594 248.5987 0000889 97.2872 262.8230 15.30191885 05
| Epoch (UTC): | 25 May 2026 13:01:17 |
| Eccentricity: | 0.0000889 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.5987° |
| argument of perigee: | 97.2872° |
| revolutions per day: | 15.30191885 |
| mean anomaly at epoch: | 262.8230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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