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 68715U 26145.58335647 +.00000000 +00000-0 -57702-1 0 00002
2 68715 53.1673 36.9384 0001077 76.9029 345.0984 15.39536441 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001077 |
| inclination: | 53.1673° |
| perigee height: | 447 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 36.9384° |
| argument of perigee: | 76.9029° |
| revolutions per day: | 15.39536441 |
| mean anomaly at epoch: | 345.0984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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