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 66316U 26145.34965083 +.00000000 +00000-0 +34549-3 0 00009
2 66316 42.0043 257.3555 0005012 115.1975 244.9370 14.99476956 05
| Epoch (UTC): | 25 May 2026 08:23:29 |
| Eccentricity: | 0.0005012 |
| inclination: | 42.0043° |
| perigee height: | 565 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 257.3555° |
| argument of perigee: | 115.1975° |
| revolutions per day: | 14.99476956 |
| mean anomaly at epoch: | 244.9370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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