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 53677U 26145.24888354 +.00000000 +00000-0 +28547-2 0 00009
2 53677 97.4474 26.3157 0002136 115.3801 244.7648 15.05434439 03
| Epoch (UTC): | 25 May 2026 05:58:23 |
| Eccentricity: | 0.0002136 |
| inclination: | 97.4474° |
| perigee height: | 549 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 26.3157° |
| argument of perigee: | 115.3801° |
| revolutions per day: | 15.05434439 |
| mean anomaly at epoch: | 244.7648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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