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 25153U 26145.21058218 +.00000000 +00000-0 +00000-0 0 00004
2 25153 9.6444 53.4885 0005112 7.3641 203.7419 1.00269244 02
| Epoch (UTC): | 25 May 2026 05:03:14 |
| Eccentricity: | 0.0005112 |
| inclination: | 9.6444° |
| perigee height: | 35766 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 53.4885° |
| argument of perigee: | 7.3641° |
| revolutions per day: | 1.00269244 |
| mean anomaly at epoch: | 203.7419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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