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 68246U 26145.42517128 +.00000000 +00000-0 +16589-2 0 00008
2 68246 53.1590 298.1067 0001131 97.5804 262.5331 15.42214970 00
| Epoch (UTC): | 25 May 2026 10:12:14 |
| Eccentricity: | 0.0001131 |
| inclination: | 53.1590° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 298.1067° |
| argument of perigee: | 97.5804° |
| revolutions per day: | 15.42214970 |
| mean anomaly at epoch: | 262.5331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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