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 61892U 26145.37151569 +.00000000 +00000-0 +27249-4 0 00002
2 61892 53.1594 131.2002 0001210 79.0952 281.0185 15.30196376 06
| Epoch (UTC): | 25 May 2026 08:54:58 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.2002° |
| argument of perigee: | 79.0952° |
| revolutions per day: | 15.30196376 |
| mean anomaly at epoch: | 281.0185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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