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 68250U 26145.42417573 +.00000000 +00000-0 +97262-3 0 00004
2 68250 53.1584 298.1019 0002202 114.7945 245.3291 15.42190044 02
| Epoch (UTC): | 25 May 2026 10:10:48 |
| Eccentricity: | 0.0002202 |
| inclination: | 53.1584° |
| perigee height: | 438 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 298.1019° |
| argument of perigee: | 114.7945° |
| revolutions per day: | 15.42190044 |
| mean anomaly at epoch: | 245.3291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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