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 64790U 26145.42364192 +.00000000 +00000-0 +17064-3 0 00009
2 64790 70.0008 300.8721 0002676 271.9677 88.1176 14.98339958 04
| Epoch (UTC): | 25 May 2026 10:10:02 |
| Eccentricity: | 0.0002676 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8721° |
| argument of perigee: | 271.9677° |
| revolutions per day: | 14.98339958 |
| mean anomaly at epoch: | 88.1176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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