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 68967U 26145.58335647 +.00000000 +00000-0 -36040-2 0 00004
2 68967 53.1593 267.8183 0001049 62.3744 164.3551 15.73862454 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001049 |
| inclination: | 53.1593° |
| perigee height: | 347 km |
| apogee height: | 349 km |
| right ascension of ascending node: | 267.8183° |
| argument of perigee: | 62.3744° |
| revolutions per day: | 15.73862454 |
| mean anomaly at epoch: | 164.3551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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