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 64274U 26145.24616221 +.00000000 +00000-0 +41643-3 0 00009
2 64274 53.1599 121.3492 0001403 134.6867 225.4248 15.30209239 03
| Epoch (UTC): | 25 May 2026 05:54:28 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.3492° |
| argument of perigee: | 134.6867° |
| revolutions per day: | 15.30209239 |
| mean anomaly at epoch: | 225.4248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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