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 68944U 26145.50969575 +.00000000 +00000-0 +32022-3 0 00000
2 68944 51.8734 177.0162 0006171 60.9069 299.2533 15.34082851 00
| Epoch (UTC): | 25 May 2026 12:13:57 |
| Eccentricity: | 0.0006171 |
| inclination: | 51.8734° |
| perigee height: | 459 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 177.0162° |
| argument of perigee: | 60.9069° |
| revolutions per day: | 15.34082851 |
| mean anomaly at epoch: | 299.2533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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