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 65578U 26145.39141815 +.00000000 +00000-0 +12472-3 0 00003
2 65578 81.3041 31.6804 0008076 253.2028 106.8244 13.84433617 00
| Epoch (UTC): | 25 May 2026 09:23:38 |
| Eccentricity: | 0.0008076 |
| inclination: | 81.3041° |
| perigee height: | 942 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 31.6804° |
| argument of perigee: | 253.2028° |
| revolutions per day: | 13.84433617 |
| mean anomaly at epoch: | 106.8244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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