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 61611U 26145.45766558 +.00000000 +00000-0 +15852-2 0 00005
2 61611 87.8858 40.7897 0001452 97.0558 263.0735 13.10376232 06
| Epoch (UTC): | 25 May 2026 10:59:02 |
| Eccentricity: | 0.0001452 |
| inclination: | 87.8858° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7897° |
| argument of perigee: | 97.0558° |
| revolutions per day: | 13.10376232 |
| mean anomaly at epoch: | 263.0735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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