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 64300U 26145.31987352 +.00000000 +00000-0 +23125-3 0 00008
2 64300 70.0018 1.3812 0003067 269.6635 90.4173 14.98338787 01
| Epoch (UTC): | 25 May 2026 07:40:37 |
| Eccentricity: | 0.0003067 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3812° |
| argument of perigee: | 269.6635° |
| revolutions per day: | 14.98338787 |
| mean anomaly at epoch: | 90.4173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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