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 68375U 26145.13279559 +.00000000 +00000-0 +27589-3 0 00005
2 68375 82.2963 38.5402 0014079 184.2024 175.9128 15.83427511 05
| Epoch (UTC): | 25 May 2026 03:11:13 |
| Eccentricity: | 0.0014079 |
| inclination: | 82.2963° |
| perigee height: | 311 km |
| apogee height: | 330 km |
| right ascension of ascending node: | 38.5402° |
| argument of perigee: | 184.2024° |
| revolutions per day: | 15.83427511 |
| mean anomaly at epoch: | 175.9128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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