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 45367U 26145.39745839 +.00000000 +00000-0 +10409-2 0 00000
2 45367 53.0438 146.7552 0006489 11.2465 348.8689 15.55104124 00
| Epoch (UTC): | 25 May 2026 09:32:20 |
| Eccentricity: | 0.0006489 |
| inclination: | 53.0438° |
| perigee height: | 397 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 146.7552° |
| argument of perigee: | 11.2465° |
| revolutions per day: | 15.55104124 |
| mean anomaly at epoch: | 348.8689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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