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 65971U 26145.12998810 +.00000000 +00000-0 +26876-3 0 00009
2 65971 41.9293 55.2250 0038663 261.7486 97.8954 15.04184365 06
| Epoch (UTC): | 25 May 2026 03:07:10 |
| Eccentricity: | 0.0038663 |
| inclination: | 41.9293° |
| perigee height: | 527 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 55.2250° |
| argument of perigee: | 261.7486° |
| revolutions per day: | 15.04184365 |
| mean anomaly at epoch: | 97.8954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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