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 68934U 26145.58335647 +.00000000 +00000-0 +14714-2 0 00001
2 68934 51.8748 177.1381 0018652 71.2585 101.4563 15.30286961 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0018652 |
| inclination: | 51.8748° |
| perigee height: | 462 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 177.1381° |
| argument of perigee: | 71.2585° |
| revolutions per day: | 15.30286961 |
| mean anomaly at epoch: | 101.4563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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