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 51777U 26145.30205601 +.00000000 +00000-0 +29571-3 0 00002
2 51777 53.2134 355.1646 0000949 59.9967 300.1120 15.08836036 01
| Epoch (UTC): | 25 May 2026 07:14:57 |
| Eccentricity: | 0.0000949 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 355.1646° |
| argument of perigee: | 59.9967° |
| revolutions per day: | 15.08836036 |
| mean anomaly at epoch: | 300.1120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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