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 64421U 26145.51460139 +.00000000 +00000-0 +24219-3 0 00008
2 64421 70.0003 240.8053 0003574 263.8421 96.2331 14.98323802 00
| Epoch (UTC): | 25 May 2026 12:21:01 |
| Eccentricity: | 0.0003574 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 240.8053° |
| argument of perigee: | 263.8421° |
| revolutions per day: | 14.98323802 |
| mean anomaly at epoch: | 96.2331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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