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 41601U 26145.09058510 +.00000000 +00000-0 +24157-3 0 00003
2 41601 96.9583 178.0678 0004455 103.9942 256.1798 15.35849586 09
| Epoch (UTC): | 25 May 2026 02:10:26 |
| Eccentricity: | 0.0004455 |
| inclination: | 96.9583° |
| perigee height: | 455 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 178.0678° |
| argument of perigee: | 103.9942° |
| revolutions per day: | 15.35849586 |
| mean anomaly at epoch: | 256.1798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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