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 68921U 26145.36628588 +.00000000 +00000-0 +13488-1 0 00008
2 68921 51.8715 177.5589 0020112 127.3545 232.9277 15.36281930 00
| Epoch (UTC): | 25 May 2026 08:47:27 |
| Eccentricity: | 0.0020112 |
| inclination: | 51.8715° |
| perigee height: | 443 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 177.5589° |
| argument of perigee: | 127.3545° |
| revolutions per day: | 15.36281930 |
| mean anomaly at epoch: | 232.9277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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