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 45572U 26144.80728729 +.00000000 +00000-0 +52549-3 0 00004
2 45572 53.0441 326.3491 0004735 271.9985 88.0494 15.82366190 04
| Epoch (UTC): | 24 May 2026 19:22:29 |
| Eccentricity: | 0.0004735 |
| inclination: | 53.0441° |
| perigee height: | 321 km |
| apogee height: | 327 km |
| right ascension of ascending node: | 326.3491° |
| argument of perigee: | 271.9985° |
| revolutions per day: | 15.82366190 |
| mean anomaly at epoch: | 88.0494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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