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 56324U 26145.46208236 +.00000000 +00000-0 +57464-4 0 00002
2 56324 97.4453 146.5901 0001294 99.5671 260.5703 15.05649646 02
| Epoch (UTC): | 25 May 2026 11:05:23 |
| Eccentricity: | 0.0001294 |
| inclination: | 97.4453° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 146.5901° |
| argument of perigee: | 99.5671° |
| revolutions per day: | 15.05649646 |
| mean anomaly at epoch: | 260.5703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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