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 61891U 26145.34055986 +.00000000 +00000-0 +10121-4 0 00005
2 61891 53.1610 130.2998 0001230 91.7417 268.3727 15.34385173 05
| Epoch (UTC): | 25 May 2026 08:10:24 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1610° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 130.2998° |
| argument of perigee: | 91.7417° |
| revolutions per day: | 15.34385173 |
| mean anomaly at epoch: | 268.3727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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