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 68167U 26145.36412500 +.00000000 +00000-0 +10682-2 0 00009
2 68167 53.1580 270.5225 0001115 99.3219 260.7912 15.38851525 06
| Epoch (UTC): | 25 May 2026 08:44:20 |
| Eccentricity: | 0.0001115 |
| inclination: | 53.1580° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 270.5225° |
| argument of perigee: | 99.3219° |
| revolutions per day: | 15.38851525 |
| mean anomaly at epoch: | 260.7912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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