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 64828U 26145.14979735 +.00000000 +00000-0 +49060-3 0 00006
2 64828 51.9018 310.0044 0000638 111.5736 248.5294 14.79937122 06
| Epoch (UTC): | 25 May 2026 03:35:42 |
| Eccentricity: | 0.0000638 |
| inclination: | 51.9018° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 310.0044° |
| argument of perigee: | 111.5736° |
| revolutions per day: | 14.79937122 |
| mean anomaly at epoch: | 248.5294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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