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 68631U 26145.54118913 +.00000000 +00000-0 +18116-3 0 00007
2 68631 60.0212 265.0505 0024438 8.7657 351.3846 15.24333812 06
| Epoch (UTC): | 25 May 2026 12:59:18 |
| Eccentricity: | 0.0024438 |
| inclination: | 60.0212° |
| perigee height: | 476 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 265.0505° |
| argument of perigee: | 8.7657° |
| revolutions per day: | 15.24333812 |
| mean anomaly at epoch: | 351.3846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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