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 68873U 26144.94165904 +.00000000 +00000-0 +68931-3 0 00000
2 68873 51.8827 354.7448 0004908 193.6263 166.4593 15.37849719 09
| Epoch (UTC): | 24 May 2026 22:35:59 |
| Eccentricity: | 0.0004908 |
| inclination: | 51.8827° |
| perigee height: | 449 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 354.7448° |
| argument of perigee: | 193.6263° |
| revolutions per day: | 15.37849719 |
| mean anomaly at epoch: | 166.4593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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