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 51850U 26153.96941720 +.00000000 +00000-0 +00000-0 0 00007
2 51850 0.0494 127.8169 0000589 346.0616 349.5498 1.00271412 00
| Epoch (UTC): | 02 June 2026 23:15:57 |
| Eccentricity: | 0.0000589 |
| inclination: | 0.0494° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 127.8169° |
| argument of perigee: | 346.0616° |
| revolutions per day: | 1.00271412 |
| mean anomaly at epoch: | 349.5498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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