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 64031U 26145.34815611 +.00000000 +00000-0 +50235-3 0 00002
2 64031 70.0006 281.2188 0003094 266.8569 93.2237 14.98352000 05
| Epoch (UTC): | 25 May 2026 08:21:20 |
| Eccentricity: | 0.0003094 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.2188° |
| argument of perigee: | 266.8569° |
| revolutions per day: | 14.98352000 |
| mean anomaly at epoch: | 93.2237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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