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 54003U 26145.51680494 +.00000000 +00000-0 -28379-4 0 00004
2 54003 53.2111 229.0302 0001365 88.3714 271.7435 15.08837414 01
| Epoch (UTC): | 25 May 2026 12:24:11 |
| Eccentricity: | 0.0001365 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 229.0302° |
| argument of perigee: | 88.3714° |
| revolutions per day: | 15.08837414 |
| mean anomaly at epoch: | 271.7435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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