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 45064U 26145.28834235 +.00000000 +00000-0 +12771-2 0 00005
2 45064 53.1551 261.3881 0003168 324.8725 35.2068 15.33738024 09
| Epoch (UTC): | 25 May 2026 06:55:12 |
| Eccentricity: | 0.0003168 |
| inclination: | 53.1551° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 261.3881° |
| argument of perigee: | 324.8725° |
| revolutions per day: | 15.33738024 |
| mean anomaly at epoch: | 35.2068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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