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 51718U 26145.55124161 +.00000000 +00000-0 +11274-2 0 00005
2 51718 53.2154 336.9549 0003820 136.1556 223.9744 15.18646121 09
| Epoch (UTC): | 25 May 2026 13:13:47 |
| Eccentricity: | 0.0003820 |
| inclination: | 53.2154° |
| perigee height: | 507 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 336.9549° |
| argument of perigee: | 136.1556° |
| revolutions per day: | 15.18646121 |
| mean anomaly at epoch: | 223.9744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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