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 68657U 26145.32764647 +.00000000 +00000-0 +11817-3 0 00003
2 68657 86.5001 51.6227 0001665 85.3236 274.8094 13.33927402 00
| Epoch (UTC): | 25 May 2026 07:51:48 |
| Eccentricity: | 0.0001665 |
| inclination: | 86.5001° |
| perigee height: | 1131 km |
| apogee height: | 1133 km |
| right ascension of ascending node: | 51.6227° |
| argument of perigee: | 85.3236° |
| revolutions per day: | 13.33927402 |
| mean anomaly at epoch: | 274.8094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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