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 54008U 26145.49930483 +.00000000 +00000-0 -89158-4 0 00004
2 54008 53.2129 218.9509 0001094 88.5208 271.5909 15.08843181 02
| Epoch (UTC): | 25 May 2026 11:58:59 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 218.9509° |
| argument of perigee: | 88.5208° |
| revolutions per day: | 15.08843181 |
| mean anomaly at epoch: | 271.5909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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