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 64829U 26145.47933323 +.00000000 +00000-0 +14365-4 0 00007
2 64829 51.9011 316.0323 0001138 115.3664 244.7416 14.79944118 01
| Epoch (UTC): | 25 May 2026 11:30:14 |
| Eccentricity: | 0.0001138 |
| inclination: | 51.9011° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 316.0323° |
| argument of perigee: | 115.3664° |
| revolutions per day: | 14.79944118 |
| mean anomaly at epoch: | 244.7416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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