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 29499U 26088.18834662 +.00000000 +00000-0 +20324-3 0 00002
2 29499 98.3254 192.4341 0173949 324.7677 94.5650 14.75644767 09
| Epoch (UTC): | 29 March 2026 04:31:13 |
| Eccentricity: | 0.0173949 |
| inclination: | 98.3254° |
| perigee height: | 521 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 192.4341° |
| argument of perigee: | 324.7677° |
| revolutions per day: | 14.75644767 |
| mean anomaly at epoch: | 94.5650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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