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 68833U 26131.62099769 +.00000000 +00000-0 +10239-3 0 00000
2 68833 55.0031 181.4760 0010474 338.0609 21.9961 15.18972133 04
| Epoch (UTC): | 11 May 2026 14:54:14 |
| Eccentricity: | 0.0010474 |
| inclination: | 55.0031° |
| perigee height: | 502 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 181.4760° |
| argument of perigee: | 338.0609° |
| revolutions per day: | 15.18972133 |
| mean anomaly at epoch: | 21.9961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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