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 63174U 26145.66810166 +.00000000 +00000-0 +50353-4 0 00006
2 63174 88.9692 302.8568 0012688 30.6886 329.5005 13.51005755 09
| Epoch (UTC): | 25 May 2026 16:02:03 |
| Eccentricity: | 0.0012688 |
| inclination: | 88.9692° |
| perigee height: | 1059 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 302.8568° |
| argument of perigee: | 30.6886° |
| revolutions per day: | 13.51005755 |
| mean anomaly at epoch: | 329.5005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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