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 67522U 26145.52999870 +.00000000 +00000-0 +81268-4 0 00001
2 67522 50.0083 77.1499 0000975 26.7482 333.3441 13.29328466 02
| Epoch (UTC): | 25 May 2026 12:43:11 |
| Eccentricity: | 0.0000975 |
| inclination: | 50.0083° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 77.1499° |
| argument of perigee: | 26.7482° |
| revolutions per day: | 13.29328466 |
| mean anomaly at epoch: | 333.3441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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