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 65570U 26145.61986736 +.00000000 +00000-0 +11769-3 0 00007
2 65570 81.3057 31.5465 0007846 254.8669 105.1620 13.84281814 03
| Epoch (UTC): | 25 May 2026 14:52:36 |
| Eccentricity: | 0.0007846 |
| inclination: | 81.3057° |
| perigee height: | 943 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 31.5465° |
| argument of perigee: | 254.8669° |
| revolutions per day: | 13.84281814 |
| mean anomaly at epoch: | 105.1620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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