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 57342U 26145.57305552 +.00000000 +00000-0 -70954-4 0 00004
2 57342 42.9999 174.8881 0001374 280.0623 80.0074 15.27588125 01
| Epoch (UTC): | 25 May 2026 13:45:11 |
| Eccentricity: | 0.0001374 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.8881° |
| argument of perigee: | 280.0623° |
| revolutions per day: | 15.27588125 |
| mean anomaly at epoch: | 80.0074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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