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 02920U 26088.10275175 +.00000000 +00000-0 +60630-4 0 00007
2 02920 98.5965 300.9558 0037147 225.7841 134.0281 14.15294395 00
| Epoch (UTC): | 29 March 2026 02:27:57 |
| Eccentricity: | 0.0037147 |
| inclination: | 98.5965° |
| perigee height: | 814 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 300.9558° |
| argument of perigee: | 225.7841° |
| revolutions per day: | 14.15294395 |
| mean anomaly at epoch: | 134.0281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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