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 25893U 26162.37176417 +.00000000 +00000-0 +68815-4 0 00005
2 25893 82.9260 101.6751 0027228 280.0446 194.5619 13.76849620 03
| Epoch (UTC): | 11 June 2026 08:55:20 |
| Eccentricity: | 0.0027228 |
| inclination: | 82.9260° |
| perigee height: | 955 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 101.6751° |
| argument of perigee: | 280.0446° |
| revolutions per day: | 13.76849620 |
| mean anomaly at epoch: | 194.5619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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