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 67435U 26145.52683385 +.00000000 +00000-0 +88414-4 0 00005
2 67435 50.0057 167.1153 0000894 283.7144 76.3628 13.29325937 04
| Epoch (UTC): | 25 May 2026 12:38:38 |
| Eccentricity: | 0.0000894 |
| inclination: | 50.0057° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.1153° |
| argument of perigee: | 283.7144° |
| revolutions per day: | 13.29325937 |
| mean anomaly at epoch: | 76.3628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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