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 64273U 26145.19340205 +.00000000 +00000-0 +87267-3 0 00000
2 64273 53.1599 121.0237 0001371 76.4171 283.6982 15.30214672 09
| Epoch (UTC): | 25 May 2026 04:38:29 |
| Eccentricity: | 0.0001371 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.0237° |
| argument of perigee: | 76.4171° |
| revolutions per day: | 15.30214672 |
| mean anomaly at epoch: | 283.6982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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