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 54152U 26145.60260462 +.00000000 +00000-0 +39821-4 0 00001
2 54152 82.5064 2.0814 0019706 280.9709 78.9154 12.42889313 02
| Epoch (UTC): | 25 May 2026 14:27:45 |
| Eccentricity: | 0.0019706 |
| inclination: | 82.5064° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 2.0814° |
| argument of perigee: | 280.9709° |
| revolutions per day: | 12.42889313 |
| mean anomaly at epoch: | 78.9154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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