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 68244U 26145.40604986 +.00000000 +00000-0 +11827-2 0 00003
2 68244 53.1594 297.9790 0000939 121.3041 238.8057 15.42200561 08
| Epoch (UTC): | 25 May 2026 09:44:42 |
| Eccentricity: | 0.0000939 |
| inclination: | 53.1594° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 297.9790° |
| argument of perigee: | 121.3041° |
| revolutions per day: | 15.42200561 |
| mean anomaly at epoch: | 238.8057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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