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 54073U 26145.55865013 +.00000000 +00000-0 +78691-4 0 00008
2 54073 53.2113 353.7005 0001312 86.9300 273.1843 15.08835086 04
| Epoch (UTC): | 25 May 2026 13:24:27 |
| Eccentricity: | 0.0001312 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 353.7005° |
| argument of perigee: | 86.9300° |
| revolutions per day: | 15.08835086 |
| mean anomaly at epoch: | 273.1843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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