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 61790U 26145.59406705 +.00000000 +00000-0 +15750-3 0 00001
2 61790 97.3258 346.5660 0006936 135.1294 225.0491 14.97778120 07
| Epoch (UTC): | 25 May 2026 14:15:27 |
| Eccentricity: | 0.0006936 |
| inclination: | 97.3258° |
| perigee height: | 569 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 346.5660° |
| argument of perigee: | 135.1294° |
| revolutions per day: | 14.97778120 |
| mean anomaly at epoch: | 225.0491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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