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 68919U 26145.48654292 +.00000000 +00000-0 -80936-3 0 00004
2 68919 51.8715 177.5941 0015121 72.8750 287.3889 15.30540514 08
| Epoch (UTC): | 25 May 2026 11:40:37 |
| Eccentricity: | 0.0015121 |
| inclination: | 51.8715° |
| perigee height: | 464 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 177.5941° |
| argument of perigee: | 72.8750° |
| revolutions per day: | 15.30540514 |
| mean anomaly at epoch: | 287.3889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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