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 45225U 26145.01591675 +.00000000 +00000-0 +11806-2 0 00001
2 45225 53.1582 3.1385 0002133 167.4587 192.6469 15.33798147 06
| Epoch (UTC): | 25 May 2026 00:22:55 |
| Eccentricity: | 0.0002133 |
| inclination: | 53.1582° |
| perigee height: | 463 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 3.1385° |
| argument of perigee: | 167.4587° |
| revolutions per day: | 15.33798147 |
| mean anomaly at epoch: | 192.6469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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