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 67246U 26145.61005280 +.00000000 +00000-0 +00000-0 0 00008
2 67246 0.0107 92.7067 0001096 50.2978 92.8073 1.00268510 05
| Epoch (UTC): | 25 May 2026 14:38:28 |
| Eccentricity: | 0.0001096 |
| inclination: | 0.0107° |
| perigee height: | 35783 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 92.7067° |
| argument of perigee: | 50.2978° |
| revolutions per day: | 1.00268510 |
| mean anomaly at epoch: | 92.8073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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