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 68012U 26145.56072297 +.00000000 +00000-0 +60572-3 0 00009
2 68012 43.0019 334.4676 0000804 281.1411 78.9350 15.27592149 06
| Epoch (UTC): | 25 May 2026 13:27:26 |
| Eccentricity: | 0.0000804 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.4676° |
| argument of perigee: | 281.1411° |
| revolutions per day: | 15.27592149 |
| mean anomaly at epoch: | 78.9350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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