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 68744U 26145.58335647 +.00000000 +00000-0 -22240-1 0 00003
2 68744 97.2848 9.2735 0001614 74.8898 346.3256 15.57464016 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001614 |
| inclination: | 97.2848° |
| perigee height: | 394 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 9.2735° |
| argument of perigee: | 74.8898° |
| revolutions per day: | 15.57464016 |
| mean anomaly at epoch: | 346.3256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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