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 68113U 26145.62071170 +.00000000 +00000-0 +56089-3 0 00005
2 68113 97.2843 106.2537 0002003 88.0226 272.1247 15.33445644 03
| Epoch (UTC): | 25 May 2026 14:53:49 |
| Eccentricity: | 0.0002003 |
| inclination: | 97.2843° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.2537° |
| argument of perigee: | 88.0226° |
| revolutions per day: | 15.33445644 |
| mean anomaly at epoch: | 272.1247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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