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 54101U 26145.49889994 +.00000000 +00000-0 +46494-4 0 00003
2 54101 53.2124 334.0718 0001173 89.8224 270.2902 15.08835217 03
| Epoch (UTC): | 25 May 2026 11:58:24 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.0718° |
| argument of perigee: | 89.8224° |
| revolutions per day: | 15.08835217 |
| mean anomaly at epoch: | 270.2902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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