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 68875U 26145.54446080 +.00000000 +00000-0 +71151-3 0 00004
2 68875 51.8784 352.0252 0007735 218.4885 141.5551 15.36888221 02
| Epoch (UTC): | 25 May 2026 13:04:01 |
| Eccentricity: | 0.0007735 |
| inclination: | 51.8784° |
| perigee height: | 450 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 352.0252° |
| argument of perigee: | 218.4885° |
| revolutions per day: | 15.36888221 |
| mean anomaly at epoch: | 141.5551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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