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 68926U 26145.47973235 +.00000000 +00000-0 -20703-2 0 00007
2 68926 51.8744 177.5544 0013905 61.7228 298.5157 15.30483295 06
| Epoch (UTC): | 25 May 2026 11:30:48 |
| Eccentricity: | 0.0013905 |
| inclination: | 51.8744° |
| perigee height: | 465 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 177.5544° |
| argument of perigee: | 61.7228° |
| revolutions per day: | 15.30483295 |
| mean anomaly at epoch: | 298.5157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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