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 64301U 26145.30319793 +.00000000 +00000-0 +44168-3 0 00006
2 64301 70.0016 1.3246 0002453 269.3860 90.7018 14.98342697 02
| Epoch (UTC): | 25 May 2026 07:16:36 |
| Eccentricity: | 0.0002453 |
| inclination: | 70.0016° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3246° |
| argument of perigee: | 269.3860° |
| revolutions per day: | 14.98342697 |
| mean anomaly at epoch: | 90.7018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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