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 02741U 26088.11629013 +.00000000 +00000-0 +91276-4 0 00003
2 02741 98.9668 39.6380 0052814 156.5732 203.7871 14.29216540 02
| Epoch (UTC): | 29 March 2026 02:47:27 |
| Eccentricity: | 0.0052814 |
| inclination: | 98.9668° |
| perigee height: | 756 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 39.6380° |
| argument of perigee: | 156.5732° |
| revolutions per day: | 14.29216540 |
| mean anomaly at epoch: | 203.7871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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