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 61741U 26145.61594258 +.00000000 +00000-0 +20539-3 0 00002
2 61741 97.3263 345.1317 0013525 135.4747 224.7564 14.96025338 03
| Epoch (UTC): | 25 May 2026 14:46:57 |
| Eccentricity: | 0.0013525 |
| inclination: | 97.3263° |
| perigee height: | 570 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 345.1317° |
| argument of perigee: | 135.4747° |
| revolutions per day: | 14.96025338 |
| mean anomaly at epoch: | 224.7564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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