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 61606U 26145.46264853 +.00000000 +00000-0 +18704-2 0 00000
2 61606 87.8875 40.6950 0001262 95.5164 264.6107 13.10374214 01
| Epoch (UTC): | 25 May 2026 11:06:12 |
| Eccentricity: | 0.0001262 |
| inclination: | 87.8875° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.6950° |
| argument of perigee: | 95.5164° |
| revolutions per day: | 13.10374214 |
| mean anomaly at epoch: | 264.6107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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