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 54002U 26145.50667457 +.00000000 +00000-0 +59512-4 0 00008
2 54002 53.2130 219.0125 0001206 86.4240 273.6890 15.08840273 03
| Epoch (UTC): | 25 May 2026 12:09:36 |
| Eccentricity: | 0.0001206 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 219.0125° |
| argument of perigee: | 86.4240° |
| revolutions per day: | 15.08840273 |
| mean anomaly at epoch: | 273.6890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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