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 51946U 26145.63692102 +.00000000 +00000-0 +63894-3 0 00008
2 51946 63.4863 346.9738 0104213 343.0498 16.7141 15.17962202 04
| Epoch (UTC): | 25 May 2026 15:17:09 |
| Eccentricity: | 0.0104213 |
| inclination: | 63.4863° |
| perigee height: | 440 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 346.9738° |
| argument of perigee: | 343.0498° |
| revolutions per day: | 15.17962202 |
| mean anomaly at epoch: | 16.7141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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