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 68032U 26145.33477855 +.00000000 +00000-0 +65235-3 0 00006
2 68032 97.2846 94.4197 0001107 101.9427 258.1940 15.33455639 07
| Epoch (UTC): | 25 May 2026 08:02:04 |
| Eccentricity: | 0.0001107 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 94.4197° |
| argument of perigee: | 101.9427° |
| revolutions per day: | 15.33455639 |
| mean anomaly at epoch: | 258.1940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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