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 68252U 26145.38775022 +.00000000 +00000-0 +11332-2 0 00000
2 68252 53.1567 296.4287 0002824 81.3440 278.7889 15.49359229 04
| Epoch (UTC): | 25 May 2026 09:18:21 |
| Eccentricity: | 0.0002824 |
| inclination: | 53.1567° |
| perigee height: | 417 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 296.4287° |
| argument of perigee: | 81.3440° |
| revolutions per day: | 15.49359229 |
| mean anomaly at epoch: | 278.7889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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