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 68333U 26145.55632015 +.00000000 +00000-0 +88816-3 0 00005
2 68333 53.1579 347.7322 0001391 99.5191 260.5975 15.49331562 04
| Epoch (UTC): | 25 May 2026 13:21:06 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.1579° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 347.7322° |
| argument of perigee: | 99.5191° |
| revolutions per day: | 15.49331562 |
| mean anomaly at epoch: | 260.5975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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