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 68726U 26145.58335647 +.00000000 +00000-0 -49604-1 0 00006
2 68726 53.1599 36.7982 0001229 105.9961 24.5665 15.42396277 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001229 |
| inclination: | 53.1599° |
| perigee height: | 438 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 36.7982° |
| argument of perigee: | 105.9961° |
| revolutions per day: | 15.42396277 |
| mean anomaly at epoch: | 24.5665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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