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 62377U 26145.59927666 +.00000000 +00000-0 +21215-3 0 00000
2 62377 45.4085 184.9126 0002169 99.1690 260.9434 14.98711717 00
| Epoch (UTC): | 25 May 2026 14:22:57 |
| Eccentricity: | 0.0002169 |
| inclination: | 45.4085° |
| perigee height: | 569 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 184.9126° |
| argument of perigee: | 99.1690° |
| revolutions per day: | 14.98711717 |
| mean anomaly at epoch: | 260.9434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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