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 68000U 26145.22608875 +.00000000 +00000-0 +12539-2 0 00005
2 68000 43.0044 336.2571 0001046 290.1750 69.8989 15.27588585 06
| Epoch (UTC): | 25 May 2026 05:25:34 |
| Eccentricity: | 0.0001046 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 336.2571° |
| argument of perigee: | 290.1750° |
| revolutions per day: | 15.27588585 |
| mean anomaly at epoch: | 69.8989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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