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 67236U 26145.40739088 +.00000000 +00000-0 +72543-4 0 00009
2 67236 50.0068 197.2419 0001003 248.3647 111.7118 13.29322710 06
| Epoch (UTC): | 25 May 2026 09:46:38 |
| Eccentricity: | 0.0001003 |
| inclination: | 50.0068° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.2419° |
| argument of perigee: | 248.3647° |
| revolutions per day: | 13.29322710 |
| mean anomaly at epoch: | 111.7118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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