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 48562U 26145.30696870 +.00000000 +00000-0 +11588-2 0 00000
2 48562 53.1559 124.9107 0007132 38.7303 321.4215 15.45394927 03
| Epoch (UTC): | 25 May 2026 07:22:02 |
| Eccentricity: | 0.0007132 |
| inclination: | 53.1559° |
| perigee height: | 425 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 124.9107° |
| argument of perigee: | 38.7303° |
| revolutions per day: | 15.45394927 |
| mean anomaly at epoch: | 321.4215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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