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 64067U 26145.58335647 +.00000000 +00000-0 +27130-3 0 00001
2 64067 43.0009 354.6102 0001685 253.7211 81.1203 15.70806529 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001685 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 354.6102° |
| argument of perigee: | 253.7211° |
| revolutions per day: | 15.70806529 |
| mean anomaly at epoch: | 81.1203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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