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 54043U 26145.49145359 +.00000000 +00000-0 +38205-3 0 00008
2 54043 34.9955 255.0569 0004482 238.2093 121.8188 15.32020296 09
| Epoch (UTC): | 25 May 2026 11:47:41 |
| Eccentricity: | 0.0004482 |
| inclination: | 34.9955° |
| perigee height: | 467 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 255.0569° |
| argument of perigee: | 238.2093° |
| revolutions per day: | 15.32020296 |
| mean anomaly at epoch: | 121.8188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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