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 57363U 26145.45335890 +.00000000 +00000-0 +33115-4 0 00009
2 57363 43.0031 167.7903 0002070 300.6927 59.3720 15.27577700 03
| Epoch (UTC): | 25 May 2026 10:52:50 |
| Eccentricity: | 0.0002070 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.7903° |
| argument of perigee: | 300.6927° |
| revolutions per day: | 15.27577700 |
| mean anomaly at epoch: | 59.3720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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