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 68397U 26145.35205926 +.00000000 +00000-0 +79649-3 0 00004
2 68397 97.2836 287.9064 0001925 53.7917 306.3504 15.33454047 02
| Epoch (UTC): | 25 May 2026 08:26:57 |
| Eccentricity: | 0.0001925 |
| inclination: | 97.2836° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 287.9064° |
| argument of perigee: | 53.7917° |
| revolutions per day: | 15.33454047 |
| mean anomaly at epoch: | 306.3504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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