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 64818U 26145.50503652 +.00000000 +00000-0 +15761-3 0 00007
2 64818 51.9006 323.4120 0000713 101.3415 258.7628 14.79935735 02
| Epoch (UTC): | 25 May 2026 12:07:15 |
| Eccentricity: | 0.0000713 |
| inclination: | 51.9006° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 323.4120° |
| argument of perigee: | 101.3415° |
| revolutions per day: | 14.79935735 |
| mean anomaly at epoch: | 258.7628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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