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 65122U 26145.61975174 +.00000000 +00000-0 +19231-3 0 00006
2 65122 49.9702 232.1352 0030274 226.4190 133.4234 14.82048181 04
| Epoch (UTC): | 25 May 2026 14:52:26 |
| Eccentricity: | 0.0030274 |
| inclination: | 49.9702° |
| perigee height: | 602 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 232.1352° |
| argument of perigee: | 226.4190° |
| revolutions per day: | 14.82048181 |
| mean anomaly at epoch: | 133.4234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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