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 61781U 26100.18024742 +.00000000 +00000-0 +24769-3 0 00004
2 61781 97.3103 329.4761 0013900 185.6602 174.4486 15.34699492 07
| Epoch (UTC): | 10 April 2026 04:19:33 |
| Eccentricity: | 0.0013900 |
| inclination: | 97.3103° |
| perigee height: | 452 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 329.4761° |
| argument of perigee: | 185.6602° |
| revolutions per day: | 15.34699492 |
| mean anomaly at epoch: | 174.4486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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