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 64620U 26144.92285469 +.00000000 +00000-0 +50311-3 0 00006
2 64620 53.1606 341.3377 0001299 96.6984 263.4164 15.30209162 07
| Epoch (UTC): | 24 May 2026 22:08:54 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 341.3377° |
| argument of perigee: | 96.6984° |
| revolutions per day: | 15.30209162 |
| mean anomaly at epoch: | 263.4164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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