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 68931U 26145.35500725 +.00000000 +00000-0 +64654-3 0 00003
2 68931 51.8745 177.4873 0001398 93.6087 266.5059 15.36495108 05
| Epoch (UTC): | 25 May 2026 08:31:12 |
| Eccentricity: | 0.0001398 |
| inclination: | 51.8745° |
| perigee height: | 456 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 177.4873° |
| argument of perigee: | 93.6087° |
| revolutions per day: | 15.36495108 |
| mean anomaly at epoch: | 266.5059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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