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 30183U 26088.08955081 +.00000000 +00000-0 +48773-3 0 00000
2 30183 98.7731 133.2690 0025017 313.2478 101.1759 14.12887942 09
| Epoch (UTC): | 29 March 2026 02:08:57 |
| Eccentricity: | 0.0025017 |
| inclination: | 98.7731° |
| perigee height: | 831 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 133.2690° |
| argument of perigee: | 313.2478° |
| revolutions per day: | 14.12887942 |
| mean anomaly at epoch: | 101.1759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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