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 45054U 26145.64320649 +.00000000 +00000-0 +10821-2 0 00007
2 45054 53.1589 282.9516 0002368 313.5192 46.5613 15.33799922 02
| Epoch (UTC): | 25 May 2026 15:26:13 |
| Eccentricity: | 0.0002368 |
| inclination: | 53.1589° |
| perigee height: | 463 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 282.9516° |
| argument of perigee: | 313.5192° |
| revolutions per day: | 15.33799922 |
| mean anomaly at epoch: | 46.5613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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