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 66981U 26145.50371381 +.00000000 +00000-0 +64537-3 0 00007
2 66981 43.0018 309.7756 0000662 296.6620 63.4163 15.27597258 04
| Epoch (UTC): | 25 May 2026 12:05:20 |
| Eccentricity: | 0.0000662 |
| inclination: | 43.0018° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 309.7756° |
| argument of perigee: | 296.6620° |
| revolutions per day: | 15.27597258 |
| mean anomaly at epoch: | 63.4163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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