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 68521U 26145.23822748 +.00000000 +00000-0 +62088-3 0 00006
2 68521 53.1582 133.7911 0000754 125.5067 234.6004 15.30208430 00
| Epoch (UTC): | 25 May 2026 05:43:02 |
| Eccentricity: | 0.0000754 |
| inclination: | 53.1582° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.7911° |
| argument of perigee: | 125.5067° |
| revolutions per day: | 15.30208430 |
| mean anomaly at epoch: | 234.6004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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