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 54777U 26145.20860395 +.00000000 +00000-0 +62251-4 0 00004
2 54777 53.2129 60.4103 0001396 80.1489 279.9660 15.08839819 08
| Epoch (UTC): | 25 May 2026 05:00:23 |
| Eccentricity: | 0.0001396 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 60.4103° |
| argument of perigee: | 80.1489° |
| revolutions per day: | 15.08839819 |
| mean anomaly at epoch: | 279.9660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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