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 64019U 26145.64918374 +.00000000 +00000-0 +78056-3 0 00002
2 64019 42.9996 283.4619 0001396 244.6562 115.4145 15.27574001 05
| Epoch (UTC): | 25 May 2026 15:34:49 |
| Eccentricity: | 0.0001396 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 283.4619° |
| argument of perigee: | 244.6562° |
| revolutions per day: | 15.27574001 |
| mean anomaly at epoch: | 115.4145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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