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 68450U 26145.39570019 +.00000000 +00000-0 +33296-3 0 00004
2 68450 97.4532 104.2118 0004085 94.3744 265.7957 15.18460342 05
| Epoch (UTC): | 25 May 2026 09:29:48 |
| Eccentricity: | 0.0004085 |
| inclination: | 97.4532° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.2118° |
| argument of perigee: | 94.3744° |
| revolutions per day: | 15.18460342 |
| mean anomaly at epoch: | 265.7957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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