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 67801U 26145.47196823 +.00000000 +00000-0 +72092-3 0 00006
2 67801 97.2871 333.4957 0002016 97.2558 262.8914 15.33452338 06
| Epoch (UTC): | 25 May 2026 11:19:38 |
| Eccentricity: | 0.0002016 |
| inclination: | 97.2871° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.4957° |
| argument of perigee: | 97.2558° |
| revolutions per day: | 15.33452338 |
| mean anomaly at epoch: | 262.8914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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