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 68051U 26145.47448006 +.00000000 +00000-0 +88792-3 0 00001
2 68051 53.1605 53.2643 0001368 92.3868 267.7290 15.30212984 07
| Epoch (UTC): | 25 May 2026 11:23:15 |
| Eccentricity: | 0.0001368 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.2643° |
| argument of perigee: | 92.3868° |
| revolutions per day: | 15.30212984 |
| mean anomaly at epoch: | 267.7290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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