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 56362U 26144.96364058 +.00000000 +00000-0 +16978-4 0 00008
2 56362 97.4489 146.0358 0002054 76.4274 283.7181 15.05654990 07
| Epoch (UTC): | 24 May 2026 23:07:38 |
| Eccentricity: | 0.0002054 |
| inclination: | 97.4489° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.0358° |
| argument of perigee: | 76.4274° |
| revolutions per day: | 15.05654990 |
| mean anomaly at epoch: | 283.7181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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