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 54244U 26145.56570169 +.00000000 +00000-0 +00000-0 0 00009
2 54244 0.0092 325.5804 0002510 62.9525 327.2744 1.00271529 02
| Epoch (UTC): | 25 May 2026 13:34:36 |
| Eccentricity: | 0.0002510 |
| inclination: | 0.0092° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 325.5804° |
| argument of perigee: | 62.9525° |
| revolutions per day: | 1.00271529 |
| mean anomaly at epoch: | 327.2744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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