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 64694U 26145.62208579 +.00000000 +00000-0 +13346-3 0 00009
2 64694 98.0567 83.3067 0001427 84.3626 275.7741 14.67554168 06
| Epoch (UTC): | 25 May 2026 14:55:48 |
| Eccentricity: | 0.0001427 |
| inclination: | 98.0567° |
| perigee height: | 668 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 83.3067° |
| argument of perigee: | 84.3626° |
| revolutions per day: | 14.67554168 |
| mean anomaly at epoch: | 275.7741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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