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 64219U 26145.01305580 +.00000000 +00000-0 +71003-3 0 00009
2 64219 53.1582 44.9142 0001047 88.3312 271.7809 15.30225364 04
| Epoch (UTC): | 25 May 2026 00:18:48 |
| Eccentricity: | 0.0001047 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.9142° |
| argument of perigee: | 88.3312° |
| revolutions per day: | 15.30225364 |
| mean anomaly at epoch: | 271.7809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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